diff --git a/CODEOWNERS b/CODEOWNERS
index 1d9c80075ed1462469f5954eb2ad669546372aa7..6283b70edad8ec27bbadca6f4318d7f4b981c0b0 100644
--- a/CODEOWNERS
+++ b/CODEOWNERS
@@ -1,5 +1,5 @@
 # Repository-specific code ownership
-  *                           @kbistreck
+  *                           @kristina.mazur
 
 # File-specific code ownership
 .gitattributes                @Florian.Schueltke
diff --git a/docs/documentation/analysis/mission_analysis/getting_started.md b/docs/documentation/analysis/mission_analysis/getting_started.md
index 2059dd0b8aa01299958b904b4ad66544ce9b201f..13a79557d9d83ad4a6c98ef4de2d0f4ca3646fb5 100644
--- a/docs/documentation/analysis/mission_analysis/getting_started.md
+++ b/docs/documentation/analysis/mission_analysis/getting_started.md
@@ -358,7 +358,7 @@ After the initial loop, we expect a robuster behavior which we can use to calcul
 
 ## Additional Output
 
-Beside the output written into the [aircraft XML](#acxml), **mission_analysis** generates a few more files you and even other tools can work with
+Beside the output written into the [aircraft XML](#acxml), **mission_analysis** generates a few more files you and even other tools can work with.
 
 
 ### Mission Data CSV {#csv_file}
@@ -396,6 +396,11 @@ Remember that nice graph from this tool's [introduction](index.md)? This is a si
 - Glidepath angle [deg]
 - Incidence angle (stabilizer) [deg]
 
+The [High Fidelity Method](methods.md/#highfi) will provide in addition:
+
+- Latitude [deg] 
+- Longitude [deg]
+
 Beside being a neat dataset to show-off, [Ecological Assessment](../ecological_assessment/index.md) can go through it to calculate the ecological impact of an aircraft flying the displayed mission.
 
 
@@ -517,7 +522,7 @@ In the `program_specific` node, you can specify if the specific air range (SAR)
 In `general` you can decide how the needed fuel is estimated and you can tell **mission_analysis** in which way it shall behave in different flight segments.
 
 
-The `mode` node lets you choose the methods that are applied. Using the keyword `low`/`mid` you will trigger the low-fidelity/mid-fidelity version of the [Standard Mission](methods.md) method. It also has three sub-methods to differentiate between `design_mission`, `study_mission` and `requirements_mission` which can be selected in the `mission_type` node. Please mind that the low-fidelity method only accepts the `design_mission`. After the first iteration, the [Weight and Balance tool](../weight_and_balance_analysis/index.md) delivers vectors containing center of gravity positions in addition to the aircraft mass (center of gravity shift due to defueling). To take that into account, you can activate `interpolate_polars`. For kerosene based propulsion, the effects are rather small, but once H2 is involved you should consider using it. Furthermore, the `rate_of_climb_switch` will only affect the [Climb to Ceiling](mission_steps.md/#climb_to_ceiling_subparagraph) step of the `requirements_mission`. With this option, **mission_analysis** calculates the optimum rate of climb towards service ceiling.
+The `mode` node lets you choose the methods that are applied. Using the keyword `low`/`mid`/`high` you will trigger the low-fidelity/mid-fidelity/high-fidelity version of the [Standard Mission](methods.md) method. It also has three sub-methods to differentiate between `design_mission`, `study_mission` and `requirements_mission` which can be selected in the `mission_type` node. Please mind that the low-fidelity method only accepts the `design_mission` and the high-fidelity method only except the study mission. After the first iteration, the [Weight and Balance tool](../weight_and_balance_analysis/index.md) delivers vectors containing center of gravity positions in addition to the aircraft mass (center of gravity shift due to defueling). To take that into account, you can activate `interpolate_polars`. For kerosene based propulsion, the effects are rather small, but once H2 is involved you should consider using it. Furthermore, the `rate_of_climb_switch` will only affect the [Climb to Ceiling](mission_steps.md/#climb_to_ceiling_subparagraph) step of the `requirements_mission`. With this option, **mission_analysis** calculates the optimum rate of climb towards service ceiling.
 
 
 Finally, in `precision` you can set the parameters which will define the before mentioned increments of your mission profile.
diff --git a/docs/documentation/analysis/mission_analysis/index.md b/docs/documentation/analysis/mission_analysis/index.md
index 8fad77ed00dd8ef6bb6fe5fe86f014dd27280a47..20ccf962554c608ffad20b260f0b1f9fb7d13ce4 100644
--- a/docs/documentation/analysis/mission_analysis/index.md
+++ b/docs/documentation/analysis/mission_analysis/index.md
@@ -31,26 +31,24 @@ Once your mission is calculated, you can choose from a wide range of profile dat
 
 | Mission method                   | mission type              | Status                                 |
 |----------------------------------|---------------------------|----------------------------------------|
-| [3D Standard Mission (low-fidelity)](methods.md/#midfi)|`design_mission::breguet`| running  :white_check_mark:|
+| [3D Standard Mission (low-fidelity)](methods.md/#midfi)|`design_mission::breguet`| running :white_check_mark:|
 | [3D Standard Mission (mid-fidelity)](methods.md/#midfi)|`design_mission`         | running :white_check_mark:|
 | [3D Standard Mission (mid-fidelity)](methods.md/#midfi)|`study_mission`          | running :white_check_mark:|
 | [3D Standard Mission (mid-fidelity)](methods.md/#midfi)|`requirements_mission`   | running :white_check_mark:|
-| [4D_trajectory (high-fidelity)](methods.md/#highfi)    |None                     | under development :construction:|
+| [4D_trajectory (high-fidelity)](methods.md/#highfi)    |`study_mission::orthodrome`| running :white_check_mark:|
 
-By now, only a [standard (3D) mission method](methods.md/#midfi) is implemented. Its mid-fidelity version can trigger the three missions mentioned above while the low-fidelity sub-version is only used for the `design_mission`. The later is a Breguet-based estimation of the consumed mission fuel and it is triggered automatically if no initial values where given for the `design_mission`. A 4D trajectory mission is also planned, but it is still in the making.
+By now, there is a [standard (3D) mission method](methods.md/#midfi) implemented providing a low-, a mid- and a high-fidelity method. Its mid-fidelity version can trigger the three missions mentioned above while the high-fidelity sub-version is only used for the `study_mission`and the low-fidelity sub-version is only used for the `design_mission`. The later is a Breguet-based estimation of the consumed mission fuel and it is triggered automatically if no initial values where given for the `design_mission`. 
 
 <pre class='mermaid'>
   graph TD;
     A[mission_analysis]-->B[design_mission]
     B-->E[low-fidelity]
     B-->F[mid-fidelity]
-    B-->G["(high-fidelity)"]
     A-->C[study_mission]
     C-->H[mid-fidelity]
-    C-->I["(high-fidelity)"]
+    C-->I[high-fidelity]
     A-->D[requirements_mission]
     D-->J[mid-fidelity]
-    D-->K["(high-fidelity)"]
 </pre>
 
 
diff --git a/docs/documentation/analysis/mission_analysis/methods.md b/docs/documentation/analysis/mission_analysis/methods.md
index 6bf67e8c90e8f19ef1ab3a56b670329abae505b9..ea6cb45d38ac88763d3bfafe117ef8503cf0964d 100644
--- a/docs/documentation/analysis/mission_analysis/methods.md
+++ b/docs/documentation/analysis/mission_analysis/methods.md
@@ -1,7 +1,7 @@
 
 # Mission Methods {#missions}
 
-Depending on computing resources and needed level of detail, we have set up three different approaches to calculate a mission. Okay... it's only two by now, but the third will come for sure! Let's see, what we can find here.
+Depending on computing resources and needed level of detail, we have set up three different approaches to calculate a mission. Let's see, what we can find here.
 
 
 ## Breguet Estimation (Low Fidelity) {#lowfi}
@@ -109,4 +109,41 @@ _FAR_FLAG_ consists of:
 
 ## 4D Trajectory (High Fidelity) {#highfi}
 
-Oops, that is not ready yet. An industrious UNICADO coder is probably working on that right now :unicorn:
+The high fidelity method works exactly as the [3D Standard Mission](#midfi) ...with one difference: it will additionally calculate the longitude and latitude of the aircraft along an Orthodrome in every mission step. For using this feature, you will need to provide information about the origin and destination airport to define the route you'd like to fly ✈️  How to do this can be checked in [Create Mission XML](../../sizing/create_mission_xml/airports.md). The coordinates will be calculated as follows: 
+
+First, the ratio $f$ of the traveled distance $r$ to the total mission distance $d$ is calculated:
+
+$$
+f = \frac{r}{d} 
+$$
+
+This ratio is used to weight the origin ($origin$) and destination ($des$) coordinates. Using the auxiliary variables $A$ and $B$, the current position is determined in Cartesian coordinates $X$, $Y$ and $Z$:
+
+<div class="mathjax-render">
+$$
+A = \frac{\sin((1 - f) \cdot d)}{\sin(d)}
+$$
+$$
+B = \frac{\sin(f \cdot d)}{\sin(d)}
+$$
+
+$$
+X = A \cdot \cos(\text{LAT}_{origin}) \cdot \cos(\text{LONG}_{origin}) + B \cdot \cos(\text{LAT}_{des}) \cdot \cos(\text{LONG}_{des})
+$$
+$$
+Y = A \cdot \cos(\text{LAT}_{origin}) \cdot \sin(\text{LONG}_{origin}) + B \cdot \cos(\text{LAT}_{des}) \cdot \sin(\text{LONG}_{des})
+$$
+$$
+Z = A \cdot \sin(\text{LAT}_{origin}) + B \cdot \sin(\text{LAT}_{des})
+$$
+</div>
+
+Finally, a conversion back to geographic coordinates (latitude $LAT$ and longitude $LONG$) is performed:
+$$
+\text{LAT} = \text{atan2}\left(Z, \sqrt{X^2 + Y^2}\right)
+$$
+$$
+\text{LONG} = \text{atan2}(Y, X)
+$$
+
+You'll find a plot of the resulting trajectory in the HTML report.
diff --git a/docs/documentation/libraries/airfoils/index.md b/docs/documentation/libraries/airfoils/index.md
new file mode 100644
index 0000000000000000000000000000000000000000..ffe1955d9521e0400cad37d4be7d8d859c240d49
--- /dev/null
+++ b/docs/documentation/libraries/airfoils/index.md
@@ -0,0 +1,92 @@
+# The `Airfoils` library
+
+**Description:**
+This file is part of UNICADO. It implements the `Airfoils` class which manages airfoil data stored in files. The class provides functionality to load airfoil files from a specified directory, print the available airfoils, retrieve airfoil polygon data, and copy airfoil files to a target directory.
+
+---
+
+## Class: Airfoils
+
+### Overview
+- **Purpose:** Manages airfoil data by loading airfoil files from a directory and providing methods to interact with them.
+- **Key Responsibilities:**
+    - Load airfoil data from a given directory.
+    - Maintain a collection (`available_airfoils`) that maps airfoil names to their file paths.
+    - Provide methods to print, retrieve, and copy airfoil data.
+
+---
+
+### Constructor
+
+#### `Airfoils(const std::filesystem::path& path_to_airfoil_directory)`
+- **Description:** Initializes the `Airfoils` object by loading airfoil files from the provided directory.
+- **Parameters:**
+    - `path_to_airfoil_directory`: Filesystem path to the directory containing airfoil files.
+- **Behavior:**
+    - Checks if the provided directory exists.
+    - If not, throws an error using `throwError` with a formatted message.
+    - Calls the private method `add_directory_airfoils(path_to_airfoil_directory)` to populate the `available_airfoils` map.
+
+---
+
+### Public Methods
+
+#### `void print_available_airfoils()`
+- **Description:** Prints the list of available airfoils with their names and file paths.
+- **Behavior:**
+    - Iterates over the `available_airfoils` map and prints each entry using formatted output.
+    - Uses `std::cout` or a runtime logging stream (`myRuntimeInfo->out`) if available.
+
+---
+
+#### `geom2::Polygon_2 get_airfoil(const std::string& airfoil)`
+- **Description:** Retrieves the polygon data of the specified airfoil.
+- **Parameters:**
+    - `airfoil`: Name of the airfoil.
+- **Return:**
+    - A `geom2::Polygon_2` object representing the airfoil's polygon data.
+- **Behavior:**
+    - Searches for the airfoil in the `available_airfoils` map.
+    - If the airfoil is not found, throws an error.
+    - Otherwise, reads and returns the airfoil data using `geom2::io::read_airfoil`.
+
+---
+
+#### `void copy_available_airfoil(const std::string& airfoil, const std::filesystem::path& target_directory)`
+- **Description:** Copies the specified airfoil file to a target directory.
+- **Parameters:**
+    - `airfoil`: Name of the airfoil.
+    - `target_directory`: Filesystem path to the destination directory.
+- **Behavior:**
+    - Checks if the target directory exists; if not, throws an error.
+    - Validates that the airfoil is available in the `available_airfoils` map; if not, throws an error.
+    - Compares the absolute paths of the source (airfoil file) and the target directory.
+        - If they are the same, logs that the copying is skipped.
+    - Attempts to copy the airfoil file using `std::filesystem::copy` with the `update_existing` option.
+    - Catches any exceptions during copying and rethrows them using `throwError`.
+
+---
+
+### Private Methods
+
+#### `void add_directory_airfoils(const std::filesystem::path& path_to_airfoil_directory)`
+- **Description:** Adds all airfoil files from the specified directory to the `available_airfoils` map.
+- **Parameters:**
+    - `path_to_airfoil_directory`: Filesystem path to the directory containing airfoil files.
+- **Behavior:**
+    - Verifies that the directory exists; if not, throws an error.
+    - Iterates over each entry in the directory using `std::filesystem::directory_iterator`.
+    - For each entry, calls the private method `add_airfoil(entry.path())`.
+
+---
+
+#### `void add_airfoil(const std::filesystem::path& airfoil_path)`
+- **Description:** Adds a single airfoil file to the `available_airfoils` map.
+- **Parameters:**
+    - `airfoil_path`: Filesystem path to the airfoil file.
+- **Behavior:**
+    - Checks if the file exists; if not, throws an error.
+    - Verifies that the path is a regular file and has a `.dat` extension.
+    - Extracts the airfoil name (using the filename's stem) and inserts it into the `available_airfoils` map.
+
+---
diff --git a/docs/documentation/libraries/aixml/endnode/getting-started.md b/docs/documentation/libraries/aixml/endnode/getting-started.md
new file mode 100644
index 0000000000000000000000000000000000000000..55c65612392f7dbcfb6d424bff44cc44aeef7715
--- /dev/null
+++ b/docs/documentation/libraries/aixml/endnode/getting-started.md
@@ -0,0 +1,45 @@
+# How to use the Endnode
+This section gives simple examples on how to use an endnode.
+
+!!! note
+    The values and variables are for tutorial purpose only
+
+## Creating and using a numeric endnode
+
+```cpp
+// Example: Create a numeric endnode for a value representing length in meters.
+Endnode<double> lengthNode("/path/to/wanted/endnode", "Aircraft Length", 10.0, "m", 5.0, 20.0);
+
+// Read from an XML node
+lengthNode.read(xml_node);
+
+// Update the value and then update the XML node
+lengthNode.set_value(12.5);
+lengthNode.update(xml_node);
+
+```
+
+## Creating and using a non-numeric endnode
+
+```cpp
+// Example: Create a string endnode for an aircraft model identifier.
+Endnode<std::string> modelNode("/path/to/string/endnode", "Aircraft Model", "A320");
+
+// Read and print the node
+modelNode.read(xml_node);
+modelNode.print();
+```
+
+## Creating and using a read-only Endnode
+```cpp
+// Example: Create a read-only endnode for a boolean
+EndnodeReadOnly<bool> readOnlyNode("/path/to/boolean/endnode");
+
+// Read the XML data
+readOnlyNode.read(xml_node);
+
+// Print both the parsed and original XML values
+// This will have only effect if it's working on a numeric node and if the numeric node is a none SI (but valid)
+readOnlyNode.print_xml();
+```
+
diff --git a/docs/documentation/libraries/aixml/endnode/index.md b/docs/documentation/libraries/aixml/endnode/index.md
new file mode 100644
index 0000000000000000000000000000000000000000..9ce745d5324d46c61607c2d18b6cd3dc1618875c
--- /dev/null
+++ b/docs/documentation/libraries/aixml/endnode/index.md
@@ -0,0 +1,137 @@
+# The `endnode` in UNICADO
+
+The `endnode` is a main access point to the aircraft exchange file and lets you interface the different nodes (leafs) in an easy way. This class is build on top of the aixml class (no inheritance) which is used for raw access of xml file content.
+
+## Overview
+
+The `endnode` implements templated classes that define an endnode as a part of an XML document. An `endnode` is the final element in a node hierarchy, representing a leaf node that contains a value and in the case of numeric nodes, its associated unit, lower and upper boundaries.
+
+The classes support:
+
+- **Numeric types** (any arithmetic type except `bool`)
+- **Boolean types** (`bool`)
+- **String type** (`std::string`)
+
+Each variant comes with its own constructors and methods to read from or update XML nodes. For numeric types, additional checks ensure that the value remains within specified boundaries and that units are valid according to SI or allowed custom conversions.
+
+## Code Structure
+
+### Concept: `is_numeric`
+
+- **Purpose:** Defines a concept that accepts arithmetic types excluding `bool`.
+- **Usage:** Used to restrict template instantiation for numeric operations.
+
+```cpp
+template <typename T>
+concept is_numeric = (std::is_arithmetic<T>::value && (!std::is_same<T, bool>::value));
+```
+
+For `std::string` and `bool` the concept is_numeric is used with logic operators:
+### For boolean:
+
+- **Purpose:** Adapts is_numeric concept that accepts bool type.
+- **Usage:** Used to restrict template instantiation for numeric operations.
+
+```cpp
+template <typename T>
+!is_numeric<T> && std::is_same<T, bool>::value
+```
+
+### For strings:
+
+- **Purpose:** Adapts is_numeric that accepts strings.
+- **Usage:** Used to restrict template instantiation for std::string operations.
+
+```cpp
+template <typename T>
+!is_numeric<T> && std::is_same<T, std::string>::value
+```
+
+
+### Class: EndnodeBase
+
+**Template Parameter:**
+
+- `T` - the type of value the endnode holds (arithmetic, bool, or std::string).
+
+**Responsibilities:**
+
+- Provides common functionality for reading XML node attributes.
+- Initializes node paths and default values.
+- Implements methods for:
+    - Reading node content from an XML node.
+    - Printing node values.
+    - Checking and converting units (for numeric types).
+    - Validating that a numeric value lies within defined boundaries.
+
+**Constructors:**
+
+- Overloaded to handle numeric types, booleans, and strings.
+- Allows setting default values, units, and boundaries.
+
+**Key Methods:**
+
+- `read(const node& xml)`: Reads XML node data.
+- `print()`: Prints the node's content.
+- `check_boundaries()`: Ensures numeric values are within allowed limits.
+- `check_unit()`: Validates unit correctness and handles custom-to-SI conversion if needed.
+- `convert_items()`: Converts values to SI units when a custom unit is used.
+
+**Internal Data Members:**
+
+- `description_`: A string description of the node.
+- `paths`: A vector of strings storing the XML path parts.
+- `value_`, `lower_boundary_`, `upper_boundary_`: Numeric values (for numeric types).
+- `unit_`: The unit associated with the numeric value.
+- Several constant collections for SI units and unit conversion factors.
+
+---
+
+### Class: Endnode
+
+**Inheritance:**
+
+- Derives from `EndnodeBase<T>`.
+
+**Purpose:**
+
+- Provides a concrete implementation of an endnode with capabilities to read from and update an XML node.
+
+**Additional Methods:**
+
+- `update(node& xml)`: Updates the XML node with the current values. Different overloads exist for numeric, boolean, and string types.
+- Overloaded arithmetic operators (`+=`, `-=`, `*=`, `/=`) for numeric types.
+- Assignment operators to easily update values or boundaries.
+- Setter methods for changing the node’s value, unit, and boundaries.
+
+**Usage Scenario:**
+
+- Use this class when you need to modify XML data – both reading from and writing to an XML document.
+
+---
+
+### Class: EndnodeReadOnly
+
+**Inheritance:**
+
+- Also derived from `EndnodeBase<T>`.
+
+**Purpose:**
+
+- Represents an XML endnode whose value is read-only after the initial XML read.
+
+**Differences from Endnode:**
+
+- Stores original XML values in separate members (`value_xml_`, `unit_xml_`, etc.).
+- Provides methods to print or retrieve the raw, unparsed XML data.
+
+**Key Methods:**
+
+- `read(const node& xml)`: Reads the XML data and stores both parsed and original (XML) values.
+- `print_xml()`: Prints the original XML values (format differs for numeric and non-numeric types).
+- Getters to access the raw XML values directly.
+
+The `EndnodeReadOnly` is mainly used for configuration files since those data should not be altered by the module. For classic access and updating, use the Endnode class.
+
+!!! danger "Important"
+    None SI units will be converted automatically to SI units by the given table in the endnode.h file when reading. Have a look at valid units in [valid units](valid_units.md)
diff --git a/docs/documentation/libraries/aixml/endnode/valid_units.md b/docs/documentation/libraries/aixml/endnode/valid_units.md
new file mode 100644
index 0000000000000000000000000000000000000000..a19850b13707462613247c3c4368a6e11ca722a9
--- /dev/null
+++ b/docs/documentation/libraries/aixml/endnode/valid_units.md
@@ -0,0 +1,59 @@
+# Allowed SI Units and how it is converted
+
+### SI Units Table
+
+| Unit   | Description                   |
+|--------|-------------------------------|
+| m      | meter                         |
+| m^2    | squaremeter                   |
+| m^3    | cubicmeter                    |
+| m/s    | meter per second              |
+| rad    | radian                        |
+| 1      | no unit                       |
+| Pa     | pascal                        |
+| kg     | kilogram                      |
+| kg/s   | kilogram per second           |
+| kg/Ns  | kilogram per newton second    |
+| s      | second                        |
+| J      | Joule                         |
+| J/kg   | Joule per kilogram            |
+| J/m^3  | Joule per cubic meter         |
+| W      | Watt                          |
+| V      | volt                          |
+| A      | ampere                        |
+| N      | newton                        |
+| N/m^2  | newton per square meter       |
+| kg/m^2 | kilogram per square meter     |
+| kg/m^3 | kilogram per cubic meter      |
+| kgm^2  | kilogram square meter         |
+| K      | Kelvin                        |
+| EUR    | Euro                          |
+| US     | Dollar                        |
+
+### Custom to SI Units Conversion Table
+
+| Custom Unit  | SI Unit |
+|--------------|---------|
+| deg          | rad     |
+| ft           | m       |
+| FL           | m       |
+| NM           | m       |
+| lbs          | kg      |
+| lbs/min      | kg/s    |
+| EUR          | EUR     |
+| US           | US      |
+| g            | 1       |
+| dBA          | Pa      |
+| EPNdB        | Pa      |
+| Sone         | Pa      |
+| h            | s       |
+| min          | s       |
+| a            | s       |
+| ft/min       | m/s     |
+| kts          | m/s     |
+| KCAS         | m/s     |
+| l            | m^3     |
+| Celsius      | K       |
+| micro meter  | m       |
+| kg/h         | kg/s    |
+
diff --git a/docs/documentation/libraries/aixml/index.md b/docs/documentation/libraries/aixml/index.md
new file mode 100644
index 0000000000000000000000000000000000000000..c1d085aa0d1bb0e2e6f55ba6e38ed917b8fc51ea
--- /dev/null
+++ b/docs/documentation/libraries/aixml/index.md
@@ -0,0 +1,11 @@
+# The aixml library
+
+This library purpose is to interact with xml files, especially for accessing xml files like the aircraft exchange file and the module configuration files.
+
+## Aixml
+
+This library contains methods for "raw" accessing of xml files based on the tinyxml library
+
+## Endnode
+
+This library contains template classes especially for the usage in UNICADO and should  be used in each C++ module for easy accessing nodes.
diff --git a/docs/documentation/libraries/index.md b/docs/documentation/libraries/index.md
index 479b8dd7febc3e2b36d5a8ef3c7fe212edb8d525..a2d47165de35b70bbd99159d54b8a4e9a804d79b 100644
--- a/docs/documentation/libraries/index.md
+++ b/docs/documentation/libraries/index.md
@@ -50,7 +50,7 @@ The **airfoils** libary provides a database for different airfoils.
 
 |Module Version|Language|License|Documentation|Dependencies|
 |:---:|:---:|:---:|---|---|
-|0.5.0|:simple-cplusplus: |GPLv3|-|-|
+|0.5.0|:simple-cplusplus: |GPLv3|[Link](airfoils/index.md)|-|
 
 ---
 
@@ -62,7 +62,7 @@ It uses a simple XML library, namely *tinyxml*, to read and parse the XML files.
 
 |Module Version|Language|License|Documentation|Dependencies|
 |:---:|:---:|:---:|---|---|
-|0.5.0|:simple-cplusplus: |GPLv3|-|-|
+|0.5.0|:simple-cplusplus: |GPLv3|[Link](aixml/index.md)|[tinyxml](https://github.com/leethomason/tinyxml2)|
 
 ---
 
@@ -105,7 +105,7 @@ The engine decks can originate from different softwaretools as long as they prov
 ## extern
 UNICADO currently uses two external libaries as submodules:
 
-- `doxygen-awesome-css` for documentation formation [(see here)](https://github.com/jothepro/doxygen-awesome-css.git)
+- `doxygen-awesome-css` for documentation formation (LEGACY - will be removed) [(see here)](https://github.com/jothepro/doxygen-awesome-css.git)
 - `pybind11` to use C++ libraries in the python tools [(see here)](https://github.com/pybind/pybind11.git)
 
 ---
@@ -135,6 +135,28 @@ The library gives a template how modules should be structured and gives helpers
 
 ---
 
+## pyavlpackage
+![Icon](site:assets/images/documentation/pymodulepackage.svg){.overview-img align=left}
+This library provides the core functionality to work with Athena Vortex Lattice (AVL) from M. Drela which is released under GPL.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|Dependencies|
+|:---:|:---:|:---:|---|---|
+|0.5.0|:simple-cplusplus: |GPLv3|-|[AVL](https://web.mit.edu/drela/Public/web/avl/)|
+
+---
+
+## pyavlunicadopackage
+![Icon](site:assets/images/documentation/pymodulepackage.svg){.overview-img align=left}
+This library provides the core functionality to work with Athena Vortex Lattice (AVL) from M. Drela which is released under GPL using the pyavlpackage and the unicado geometry based on aircraftgeoemtry2.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|Dependencies|
+|:---:|:---:|:---:|---|---|
+|0.5.0|:simple-cplusplus: |GPLv3|-|[AVL](https://web.mit.edu/drela/Public/web/avl/)|
+
+---
+
 ## pymodulepackage
 ![Icon](site:assets/images/documentation/pymodulepackage.svg){.overview-img  align=left}
 This library provides standardized UNICADO data preprocessing, run, and postprocessing functions for Python modules.
@@ -196,4 +218,4 @@ In addition, it defines some common **constants** which are useful for calculati
 
 |Module Version|Language|License|Documentation|Dependencies|
 |:---:|:---:|:---:|---|---|
-|0.5.0|:simple-cplusplus: |GPLv3|-|-|
\ No newline at end of file
+|0.5.0|:simple-cplusplus: |GPLv3|-|-|
diff --git a/docs/documentation/sizing/create_mission_xml/airports.md b/docs/documentation/sizing/create_mission_xml/airports.md
new file mode 100644
index 0000000000000000000000000000000000000000..864b1664083ab7cd375b8050f24f47564476dcdd
--- /dev/null
+++ b/docs/documentation/sizing/create_mission_xml/airports.md
@@ -0,0 +1,28 @@
+# Airports
+
+The module provides the possibility to define an origin and destination airport of a study mission. If you use this, the module will read the location of the airports from a database, calculate the shortest distance (Orthodrome) between them and write those information to the [output xml file](getting_started.md#output). This is a nice feature, as it allows [Mission Analysis](../../analysis/mission_analysis/index.md) to calculate the location of the aircraft in every mission step for a designated route. While it is not a necessary information in the aircraft design process, for a detailed ecological assessment it is essential to know where exactly the aircraft operates.
+
+To use this feature, you need to enable the switch `airports/enable` within the study_mission part of the [Configuration File](getting_started.md#config_file). Then you can define the airports via their ICAO or IATA code. In total, there are more than 5000 airports available in the database. If you're interested to see the list or would like to add your own airport, have a look into the airports.csv located in the `create_mission_xml_lib`-folder next to the executable. The list is based on data published [here](https://github.com/dedolist/open-data/blob/master/data/locations/airports/data.csv) under the [Open Data Commons Public Domain Dedication and License (PDDL) v1.0](https://opendatacommons.org/licenses/pddl/1-0/index.html) and you're free to extend or change this data.
+
+If you provide two existing airport codes, the module will calculate the Orthodrome between the airports via the Haversine formula [@Ple24]:
+<div class="mathjax-render">
+$$
+\chi = \sin^2\left(\frac{\Delta \text{LAT}}{2}\right) + \cos(\text{LAT}_A) \cdot \cos(\text{LAT}_B) \cdot \sin^2\left(\frac{\Delta \text{LONG}}{2}\right) 
+$$
+
+$$
+D = (R + H) \cdot 2 \cdot \text{arctan2}\left( \sqrt{\chi}, \sqrt{1 - \chi} \right)
+$$
+</div>
+
+where:
+
+- $D$: Distance between airports [m]
+- $R$: Radius of the Earth [m]
+- $H$: Initial flight altitude [m]
+- $\text{LAT}$: Latitude in radians
+- $\Delta \text{LAT} = \text{LAT}_A - \text{LAT}_B$
+- $\text{LONG}$: Longitude in radians
+- $\Delta \text{LONG} = \text{LONG}_A - \text{LONG}_B$
+- $A$: Departure airport
+- $B$: Destination airport
\ No newline at end of file
diff --git a/docs/documentation/sizing/create_mission_xml/getting_started.md b/docs/documentation/sizing/create_mission_xml/getting_started.md
index 09a1284039baa0b073626a7021837aae57100dd1..326688286ea47c5655071eea4e73482db18bfbf3 100644
--- a/docs/documentation/sizing/create_mission_xml/getting_started.md
+++ b/docs/documentation/sizing/create_mission_xml/getting_started.md
@@ -77,8 +77,10 @@ program_settings
 │   ├── alternate_distance
 │   ├── engine_warmup_time
 │   ├── taxiing_procedure
-│   ├── origin_airport
-│   ├── destination_airport
+│   ├── airports
+│   │   ├── enable
+│   │   ├── origin_airport
+│   │   ├── destination_airport
 ├── study_mission
 │   ├── copy_mach_number
 │   ├── copy_initial_cruise_altitude
@@ -96,17 +98,19 @@ program_settings
 │   ├── alternate_distance
 │   ├── engine_warmup_time
 │   ├── taxiing_procedure
-│   ├── origin_airport
-│   ├── destination_airport
+│   ├── airports
+│   │   ├── enable
+│   │   ├── origin_airport
+│   │   ├── destination_airport
 ```
 
-In this config, you can decide what takeoff and approach procedure you want to use and how the aircraft shall operate at the airport and while cruising. In the `mission_selector`, you can choose if the `mission file` shall be generated for a `design_mission`, `study_mission` or `requirements_mission`. For more details, check the descriptions in `create_mission_xml_conf.xml`.
+In this config, you can decide what takeoff and approach procedure you want to use and how the aircraft shall operate at the airport and while cruising. In the `mission_selector`, you can choose if the `mission file` shall be generated for a `design_mission`, `study_mission` or `requirements_mission`. You can also define the origin and destination airport in case you'd like get detailed trajectory information of [Mission Analysis](../../analysis/mission_analysis/index.md). For more details on possible settings, check the descriptions in `create_mission_xml_conf.xml`.
 
 !!!node
     `maximum_operating_mach_number` and the nodes starting with `auto` will lead to **mission_analysis** ignoring user input from the aircraft XML. In those cases, the tool will try to find an own optimum.
 
 
-## Output
+## Output {#output}
 
 Like we have already discussed, the output of **create_mission_xml** is the mission_file which generally looks like this:
 
@@ -175,6 +179,42 @@ Like we have already discussed, the output of **create_mission_xml** is the miss
     <taxiing_procedure description="Taxiing procedure for start and landing.">
         <value>propulsion_taxiing</value>
     </taxiing_procedure>
+        <airports>
+        <origin>
+            <code description="ICAO or IATA code of origin airport">
+                <value>HAM</value>
+            </code>
+            <longitude description="Longitude of origin airport">
+                <value>0.1743274648</value>
+                <unit>rad</unit>
+                <lower_boundary>-3.15</lower_boundary>
+                <upper_boundary>3.15</upper_boundary>
+            </longitude>
+            <latitude description="Latitude of origin airport">
+                <value>0.9360268661</value>
+                <unit>rad</unit>
+                <lower_boundary>-1.58</lower_boundary>
+                <upper_boundary>1.58</upper_boundary>
+            </latitude>
+        </origin>
+        <destination>
+            <code description="ICAO or IATA code of origin airport">
+                <value>FRA</value>
+            </code>
+            <longitude description="Longitude of destination airport">
+                <value>0.1495826754</value>
+                <unit>rad</unit>
+                <lower_boundary>-3.15</lower_boundary>
+                <upper_boundary>3.15</upper_boundary>
+            </longitude>
+            <latitude description="Latitude of destination airport">
+                <value>0.8732459244</value>
+                <unit>rad</unit>
+                <lower_boundary>-1.58</lower_boundary>
+                <upper_boundary>1.58</upper_boundary>
+            </latitude>
+        </destination>
+    </airports>
     <departure description="Departure procedure; Additional nodes neded for mode... 
                                 Takeoff: No additional nodes. 
                                 climb: End Point Altitude [m] (double).
@@ -273,16 +313,19 @@ Like we have already discussed, the output of **create_mission_xml** is the miss
 </mission>
 ```
 
-!!!node
+!!!note
     Bleed air and power offtakes are not displayed here, but every step will include these, too. Offtakes are written and explained by [Systems Design](../systems_design/index.md).
 
+!!!note
+    The airport information will only be written for the study mission and only if you've enabled the aircraft switch in the configuration file!
+
 
-While the most parameters like `range` and `alternate_distance` are copied directly from [Aircraft Exchange File](#acxml) and [Configuration File](#config_file), the `payload` is derived from the given number of passengers, their luggage and the mass per passenger. Each step (`departure_step`, `cruise_step` or `approach_step`) contains the nodes `configuration`, `mode`, `derate` and `rating`. The `configuration` node will tell [Mission Analysis](../../analysis/mission_analysis/index.md) which polar (generated by [Aerodynamic Assessment](../../analysis/aerodynamic_analysis/index.md)) shall be used. `derate` and `rating` characterize the engine operations and `mode` specifies what shall happen during the segment between two steps (more infos about `modes`, [click here](../../analysis/mission_analysis/mission_steps.md/#step_modes)). Furthermore, `cruise_steps` always include `flight_management_system` and `auto_select_optimum_flight_level` nodes.
+While the most parameters like `terminal_operation_time` and `alternate_distance` are copied directly from [Aircraft Exchange File](#acxml) and [Configuration File](#config_file), the `payload` is derived from the given number of passengers, their luggage and the mass per passenger. The `range`is either copied from the [Aircraft Exchange File](#acxml), or calculated as described in [Airports](airports.md). Each step (`departure_step`, `cruise_step` or `approach_step`) contains the nodes `configuration`, `mode`, `derate` and `rating`. The `configuration` node will tell [Mission Analysis](../../analysis/mission_analysis/index.md) which polar (generated by [Aerodynamic Assessment](../../analysis/aerodynamic_analysis/index.md)) shall be used. `derate` and `rating` characterize the engine operations and `mode` specifies what shall happen during the segment between two steps (more infos about `modes`, [click here](../../analysis/mission_analysis/mission_steps.md/#step_modes)). Furthermore, `cruise_steps` always include `flight_management_system` and `auto_select_optimum_flight_level` nodes.
 
 Other entries within these steps can differ depending on which `mode` is used. What input nodes are needed can be found in the descriptions of `departure`, `cruise` and `approach`. As a rule of thumb, the following input nodes can usually be expected:
 
 - `mode` that changes speed: Target speed (Mach or CAS), rate of climb or target speed
 - `mode` that changes altitude: Target altitude, rate of climb or target speed
 
-!!!node
+!!!note
     For an `approach_step`, the rate of climb cannot be determined up-front, because the glide path angle must be kept constant at $3°$ due to regulatory requirements. Therefore, the rate of climb will be derived from the `glide_path` node by [Mission Analysis](../../analysis/mission_analysis/index.md).
diff --git a/docs/documentation/sizing/wing_design/design-methods.md b/docs/documentation/sizing/wing_design/design-methods.md
index 6d8e1f0a2c336670c4f35d159967f6a95fb6b4a2..323feb1389904d243e71d8bc52f71721e3673827 100644
--- a/docs/documentation/sizing/wing_design/design-methods.md
+++ b/docs/documentation/sizing/wing_design/design-methods.md
@@ -36,7 +36,7 @@ If the limits are exceeded which are defined in the aircraft exchange file in th
 After computing the aspect ratio, the taper ratio can be user defined or determined by a method from Howe. Howe uses the aspect ration and the quarter chord sweep to compute the taper ratio.
 
 #### Step 5: Dihedral computation
-The next step computes the dihedral which can be set by user or will be computed based on limits defined by Howe or Raymer. Since both, Howe and Raymer just give limitations, the dihedral as a mean value between the minimum and maximum values. Howe differentiates between sweept and unsweept while Raymer includes the mach state of the aircraft.
+The next step computes the dihedral which can be set by user or will be computed based on limits defined by Raymer. Raymer only defines limitations, so the dihedral is calculated as a mean value between the minimum and maximum values. Raymer differentiates between swept and unswept, including the mach state (transonic / supersonic) of the aircraft.
 
 #### Step 6: Calculate geometry
 Based on the computed data and the information from the aircraft exchange file, it will be determined if the wing geometry will be calculated with a kink or not. The kink is enabled when the _landing gear_ is _wing mounted_ and the wing is mounted _low_. Otherwise it uses an unkinked geometry.
@@ -49,6 +49,6 @@ The unkinked geometry calculation is straight forward, however the kinked versio
 The spar positions and control devices can be set by user. For control devices, a basic set of control devices will be set consisting of an aileron, and a number of high lift devices and spoilers for air and ground.
 
 #### Step 8: Mass calculation
-With the wing finished, the mass of the wing will be computed by two different methods, one is the Flight Optimization System (Flops) method and the other is a Method from Chiozzotto (PhD Thesis). Both methods allow changes in material while Flops uses a factor from 0 to 1 to vary the ratio between aluminim and composite materials while Chiozzotto sets two materials - _AL_ for aluminium and _CFRP_ for carbon fibre reinforced plastics.
+With the wing finished, the mass of the wing will be computed by two different methods, one is the Flight Optimization System (Flops) method and the other is a Method from Chiozzotto (PhD Thesis). Both methods allow changes in material while Flops uses a factor from 0 to 1 to vary the ratio between aluminum and composite materials while Chiozzotto sets two materials - _AL_ for aluminum and _CFRP_ for carbon fibre reinforced plastics.
 
 For the determination of the center of gravity and the position, again empirical methods from Howe are used.
diff --git a/docs/documentation/sizing/wing_design/index.md b/docs/documentation/sizing/wing_design/index.md
index d60a3ecd22277dc877d1484930eb6f33e26730e9..d8d1eb12a1c1dd2f86b79523fe760b5e4ad8d34d 100644
--- a/docs/documentation/sizing/wing_design/index.md
+++ b/docs/documentation/sizing/wing_design/index.md
@@ -1,5 +1,5 @@
 # Introduction {#mainpage}
-The wing is an essential part of an aircraft, therefore the _wing\_design_ tool is one of the core design tools in UNICADO and enables the workflow to design wings according to specified requirements and design specifications. 
+The wing is an essential part of an aircraft, therefore the _wing\_design_ tool is one of the core design tools in UNICADO and enables the workflow to design wings according to specified requirements and design specifications.
 
 According to the workflow, the tool requires a valid _Aircraft Exchange File_ with inputs from the tools _initial\_sizing_ and _fuselage\_design_.
 
@@ -17,20 +17,20 @@ According to the workflow, the tool requires a valid _Aircraft Exchange File_ wi
 ## Summary of features
 Here is a quick overview of what the tool is currently capable of including a preview which is planned:
 
-| Configuration     | Wing Type  | Methods |                           Status |
-|-------------------|------------|---------|:---------------------------------:|
-| tube-and-wing     | Cantilever | TUB     |       running :white_check_mark: |
-| blended-wing-body | ...        | ...     | under development :construction: |
+| Configuration     | Wing Type  | Methods |                 Status                  |
+|-------------------|------------|---------|:---------------------------------------:|
+| tube-and-wing     | Cantilever | TUB     | running :octicons-feed-issue-closed-16: |
+| blended-wing-body | ...        | ...     |    under development :construction:     |
 
 ## A User's Guide to Wing Design
 The _wing\_design_ tool will help you design various wings for classical configurations to blended wing body configurations (in the future). This user documentation will guide you through all necessary steps to understand the tool as well as the necessary inputs and configurations to create a new wing from scratch.
 
 The following pages will guide you through the process of generating your first wing within UNICADO:
 
-[:octicons-arrow-right-16: Basic Concepts](basic-concepts.md)   
-[:octicons-arrow-right-16: Getting Started](getting-started.md)   
-[:octicons-arrow-right-16: Design Methods](design-methods.md)   
-[:octicons-arrow-right-16: Design your first wing](run-your-first-wing-design.md)   
+[:octicons-arrow-right-16: Basic Concepts](basic-concepts.md)
+[:octicons-arrow-right-16: Getting Started](getting-started.md)
+[:octicons-arrow-right-16: Design Methods](design-methods.md)
+[:octicons-arrow-right-16: Design your first wing](run-your-first-wing-design.md)
 
 So let's get started!
 
@@ -41,10 +41,10 @@ If you are familiar with these concepts and want to contribute - head over to th
 
 The following pages will help you understand the build process code structure:
 
-[:octicons-arrow-right-16: Prerequisites](prerequisites.md)   
-[:octicons-arrow-right-16: Build the code](../../../get-involved/build-instructions/build/python.md)   
-[:octicons-arrow-right-16: Wing module structure](module-structure.md)   
-[:octicons-arrow-right-16: Method template](method-template.md)   
+[:octicons-arrow-right-16: Prerequisites](prerequisites.md)
+[:octicons-arrow-right-16: Build the code](../../../get-involved/build-instructions/build/python.md)
+[:octicons-arrow-right-16: Wing module structure](module-structure.md)
+[:octicons-arrow-right-16: Method template](method-template.md)
 
 We appreciate it!
 
diff --git a/docs/get-involved/modularization/cpp-modularization.md b/docs/get-involved/modularization/cpp-modularization.md
index 290726f7028be621aedecd7c1d182e9da737af05..7acf710dc35d7bac9a7af3fecd91341937fb9528 100644
--- a/docs/get-involved/modularization/cpp-modularization.md
+++ b/docs/get-involved/modularization/cpp-modularization.md
@@ -64,11 +64,11 @@ The class provides several public methods for various operations:
 
 - `showRuntime()` - Prints runtime information, e.g. program name, enabled flags etc.
 - `showDirectories()` - shows stored directories in directories_ map.
-- `getIODir()`, `getGeometryDir()` and other similar functions which return the path w/o ending seperator
-- `createGeometryDir()`, `createAirfoilDataDir()` and other similar functions which create the directoryif not existent
+- `getIODir()`, `getGeometryDir()` and other similar functions which return the path w/o ending separator
+- `createGeometryDir()`, `createAirfoilDataDir()` and other similar functions which create the directory if not existent
 - `checkFileExistence()` - checks if a file exists by specific argument
 - `create_common_directories` - creates standard output directories if not existent
-- `addDir()` - adds a directory to the directories_ map and creates it if not existent. The key will be specified in upper case letters
+- `add_directory()` - adds a directory to the directories_ map and creates it if not existent. The key will be specified in upper case letters
 - `reopenAcXML()` - reopens the aircraftXML - please make sure to (save and) close the acxml before
 - `saveAcXML()` - saves the current acxml node from the runtimeIO instantiation
 - `closeAcXML()` - closes the current acxml node from the runtimeIO instantiation
@@ -232,13 +232,14 @@ modeSelection = Modeselector("mode_2")
 modi selectedMode = modeSelection.get(); // selectedMode = 2
 ```
 
-## Intermediate level
+## Intermediate level (Virtual) and low level
 
-### Strategy and StrategySelector
+The intermediate level is at the current state a virtual level which routes you to your desired strategy (called so, since we use the strategy pattern to define it). However, the strategy itself specifies a new method which can be integrated. The intermediate level itself just describes the route to it. So you can think of it as a tree.
+The low level actual implements the new strategy (or method, however you want to call it for yourself). Since intermediate level and low level are somewhat connected, we will show what you need to create a new _strategy_ and how you can run such a strategy from the top level using the so called `StrategySelector`.
 
-The intermediate level, which describes the routing from top to low level, uses the so called **Strategy Design Pattern**. This pattern allows to set a specific strategy at first place and let it run through Selector, in this case the `StrategySelector` class (`strategySelector.h`, header-only).
+### Strategy
 
-Each strategy, such as the low-fidelity strategy or high-fidelity strategy, is implemented as a class that inherits from the base class `Strategy`. The `Strategy` base class defines the following pure virtual methods:
+Each strategy, such as e.g. a low-fidelity strategy or a high-fidelity strategy, is implemented as a class that inherits from the base class `Strategy`. The `Strategy` base class defines the following pure virtual methods which is defined inside the `strategySelector.h` header:
 
 - `initialize()`
 - `run()`
@@ -259,48 +260,11 @@ public:
     virtual void save() = 0;
     virtual ~Strategy() {};
 };
-```
-The `StrategySelector` class serves as a selector for strategies. It manages a dynamic allocation of a strategy using a `std::unique_ptr`. The class provides member functions to set the strategy, initialize the strategy with a given configuration class, run, update, report and save the strategy. Methods for this are:
 
-- `setStrategy()`
-- `initializeStrategy()`
-- `runStrategy()`
-- `updateStrategy()`
-- `reportStrategy()`
-- `saveStrategy()`
 
-The code for the class:
+The Strategy class is given as a basic template which should be used. However, an adaption of Input/Output types might be necessary but must be clearly stated.
 
-```c++
-class StrategySelector
-{
-public:
-    void setStrategy(std::unique_ptr<Strategy> strategy) {
-        strategy_ = std::move(strategy);
-    }
-    void initializeStrategy() {
-        strategy_->initialize();
-    }
-    void runStrategy() {
-        strategy_->run();
-    }
-    void updateStrategy() {
-        strategy_->update();
-    }
-    void reportStrategy() {
-        strategy_->report();
-    }
-    void saveStrategy() {
-        strategy_->save();
-    }
-private:
-    std::unique_ptr<Strategy<> strategy_;
-};
-```
-
-The Strategy and StrategySelector classes are given as basic templates which should be used. However, an adaption of Input/Output types might be necessary but must be clearly stated.
-
-To use these classes, a minimal example can be seen below:
+To use the class, a minimal example can be seen below:
 
 ```c++
 #include "strategySelector.h"
@@ -316,7 +280,7 @@ public:
 	void report() { std::cout << "report low" << std::endl; }
 	void save() { std::cout << "save low" << std::endl; }
 
-        const std::shared_ptr<RuntimeIO>& rtIO;
+  const std::shared_ptr<RuntimeIO>& rtIO;
 };
 
 class High : public Strategy
@@ -331,81 +295,56 @@ public:
 
 	const std::shared_ptr<RuntimeIO>& rtIO;
 };
+```
 
-int main(void) {
+Here, we have two strategies - a `low` strategy and a `high` strategy which inherit the base class `Strategy` and implement the necessary pure virtual methods. So we've now the low level and the top level. How to get to one of the strategies right now? Here the `StrategySelector` class will be introduced:
 
-	StrategySelector strategyholder;
-        const std::shared_ptr<RuntimeIO> rtIO = std::make_shared<RuntimeIO>(.....);
-	strategyholder.setStrategy(std::make_unique<Low>(rtIO));
+The `StrategySelector` class serves as a selector for strategies. It manages a dynamic allocation of a strategy using a `std::unique_ptr`. The class provides two major functions which will do the job you want to get to the strategy you want:
 
-	strategyholder.runStrategy();
+- `registerStrategy<strategy>(std::vector<std::string>)` - registers the `strategy` under a specific path defined by a vector of strings
+- `setStrategy(std::vector<std::string> , std::shared_ptr<RuntimeIO>)` - sets a registered strategy based on a vector of strings and an instance of a smart pointer of RuntimeIO.
 
-	strategyholder.setStrategy(std::make_unique<High>());
-	strategyholder.runStrategy();
-	strategyholder.saveStrategy();
-	return 0;
-}
-```
+The first method allows you to set up the method you want and the second allows you to set the method you want to use. So we go a step further and setup the example for the `Low` and `High` strategy:
 
-Output generated:
+```c++
+int main(void) {
 
-```bash
-$ ./a.exe
-run low
-run high
-save high
-```
-With `setStrategy`, a strategy will be selected and the RuntimeIO shared smart pointer is handed over to the strategy as a reference. All other calls via `strategyholder` will call methods from the *Low class strategy*. However, the strategy is changed after the first call of `runStrategy`, so below that second `setStrategy` statement, Methods within *High Strategy* are called.
+  // Define the strategyselector as strategy
+	StrategySelector strategy;
 
-The strategy is selected via a routing table system. To improve readability for the routing table, the file `strategySelector.h` provides two overlays:
+  // Get an RuntimeIO instance as a smart shared pointer
+  const std::shared_ptr<RuntimeIO> rtIO = std::make_shared<RuntimeIO>(.....);
 
-- `strategyptr` - `std::unique_ptr<Strategy>(const std::shared_ptr<RuntimeIO>&`
-- `strategyaccess` - `std::function<strategyptr>`
+  // Register your strategy by defining a path to the associated
+  strategy.registerStrategy<Low>({"low"})
+  strategy.registerStrategy<High>({"high"})
 
-A routing table is defined in a method inside the derived module class. As an example for empennage_design:
+  // Sets the strategy - here hardcoded selection of "high"
+  strategy.setStrategy({"high"}, rtIO);
 
-```c++
-strategyaccess EmpennageDesign::routing_(const std::vector<std::string>& route) {
-
- /* Routing table */
- std::map<std::string,std::map<std::string,std::map<std::string,strategyaccess>>> table = {
-   {"TAW",
-     std::map<std::string,std::map<std::string,strategyaccess>>{
-       {"CONVENTIONAL",
-         std::map<std::string,strategyaccess>{
-           {"LOW",[](const std::shared_ptr<RuntimeIO>& arg) {return std::make_unique<LowConventionalTaw>(arg);}},
-         }
-       },
-     }
-   },
-   {"BWB",
-     std::map<std::string,std::map<std::string,strategyaccess>>{
-       {"FINS",
-         std::map<std::string,strategyaccess>{
-           {"LOW",[](const std::shared_ptr<RuntimeIO>& arg) {return std::make_unique<LowFinsBwb>(arg);}},
-           {"MID",[](const std::shared_ptr<RuntimeIO>& arg) {return std::make_unique<MidFinsBwb>(arg);}}
-         }
-       }
-     }
-   }
- };
-
- return table[route.at(0)][route.at(1)][route.at(2)];
+  // Afterwards you can run also any of the implemented pure virtual methods which are defined in the currently set strategy like
+  strategy.runStrategy()
+	return 0;
 }
 ```
 
-`[](const std::shared_ptr<RuntimeIO>& arg) {return std::make_unique<LowFinsBwb>(arg)` is a lambda function which handle is returned from the routing_ table.
+With `setStrategy`, a strategy will be selected and the RuntimeIO shared smart pointer is handed over to the strategy as a reference.
 
 Inside the module constructor, the strategy is set by
 
 ```c++
-EmpennageDesign::EmpennageDesing(...) : Module(...) {
-  // read route from configuration file and store into std::vector<std::string> route_; name of vector might differ if there are more than one strategy to call
-  strategy_.setStrategy(routing_(route)(rtIO_));
+EmpennageDesign::EmpennageDesign(...) : Module(...) {
+  // read route from configuration file and store into std::vector<std::string> route; name of vector might differ if there are more than one strategy to call
+  std::vector<std::string> route = ... // Directly set up route - might not be necessary
+  ...
+  // Strategy registration
+  strategy.registerStrategy<...>(...);
+  ...
+  strategy.setStrategy(route, rtIO_);
   ...}
 ```
 
-The parameter for strategy set is called by invoking `routing_(...)` with the `route` vector which returns the handle for the selected strategy from the routing table according to the route. With `...(rtIO_)`, the returned handle is called with the `RuntimeIO` object `rtIO_` as an argument. The result is than handed over to the setStrategy method.
+The routing is done via a vector of `std::string` which can be anything (like keywords defining the aircraft type, the fidelity level of your method/strategy, the aircraft configuration or anything else). These strings build up the tree for the selection. If there is a registered strategy under such a vector string, you can access the strategy via setStrategy. Otherwise you get an error that the desired method is not existing.
 
 If you'd like to add your own module, you can choose the structure of your routing table freely. Existing UNICADO modules use for example following layers:
 
@@ -415,30 +354,29 @@ If you'd like to add your own module, you can choose the structure of your routi
 - method name
 - ...
 
-### The Fidelities {#fidelities}
+??? info "Fidelities"
+    The modularization was introduced for different fidelities. However this might not fit for all modules. If you have methods/strategies for certain fidelities, please stick to our fidelity list:
 
-The fidelity of each methods can be classified as low, mid, higher, high and own as follows:
+      - `low` - empirical methods
+      - `mid` - semi-empirical methods
+      - `higher` - analytical methods
+      - `high` - numerical methods
+      - `own` - own method (experimental)
 
-- `low` - empirical methods
-- `mid` - semi-empirical methods
-- `higher` - analytical methods
-- `high` - numerical methods
-- `own` - own method (experimental)
-
-## Low level
-
-!!!note
+### The low level
+This is a short recap of the former description. Make sure to have the strategy pure virtuals with you.
+??? note
     The low level implementations members should be public only. This has different reasons:
 
     1. There is no method next to the current
     2. To keep the overhead of the class as small as possible (no setter/getter methods which must be provided for private members)
-    3. Due to pep8 conventions (python normally has no private / protected members)
+    3. Due to pep8 conventions (python normally has no private / protected members) - yes naming convention is pep8 (even if it is not handled everywhere correctly, since it started somewhere else)
     4. isocpp: all private or all public - no mixture
 
 On the low level, the implementation of the algorithms is focused. Here you can structure your implementations according to the five base methods:
 
 - `initialize` - initialize your module to your needs and your output data by reading and preparing the data.
-- `run` - Here happens your wizardy stuff, sometimes muggle-like, sometime not 🧙.
+- `run` - Here happens your wizardly stuff, sometimes muggle-like, sometime not 🧙.
 - `update` - lets you call the update methods within the IOData class
 - `save` - if you opened any specific document during your module execution, you can save the data within this method and close the data.
 
@@ -490,12 +428,15 @@ public:
 /* LOW FIDELITY CONFIGS END */
 ```
 
+To see an example for this, have a look at `wing_design` module or `empennage_design` module.
+
+
 ### Report
 
 For report generation, a dedicated Report class (`report.h`) can be used. It offers access to HTML and Tex streams. Public methods are the following:
 
 - `Report` - Constructor
-- `setAircraftName` - Set the aircraftname for report documents
+- `setAircraftName` - Set the aircraft name for report documents
 - `generateReports` - generates reports based on settings from RuntimeIO (in case a module writes more than one report, individual names can be used)
 - `htmlReportStream` - returns the html report output stream
 - `texReportStream` - returns the tex report output stream
@@ -504,7 +445,7 @@ For report generation, a dedicated Report class (`report.h`) can be used. It off
 - `reportName` - returns standard name of the report
 - Legacy Method `addPlot` - adds a plot to the plots map by the name of the plot in case `plot.h` is used
 
-All methods for a report must be on the low level for a specific fidelity in a seperate `...Report.cpp` File. Report is an object of the main specific fidelity class and NOT an inherited class. Within your html report, can add generated plots by using the `image` function of `html.h`
+All methods for a report must be on the low level for a specific fidelity in a separate `...Report.cpp` File. Report is an object of the main specific fidelity class and NOT an inherited class. Within your html report, can add generated plots by using the `image` function of `html.h`
 
 ### Plot
 !!!attention
@@ -523,11 +464,13 @@ The Plot class (`plot.h`) is a basic frame for SVG Plot generation. There are mu
 - `generatePlotScript` - Generates plot script which is in the script stringstream
 - `generateSvg` - generates .svg based on the plotname in the given directory based on reference of a vector of unique pointers which stores svgObjects.
 
-All methods for a report must be on the low level for a specific fidelity in a seperate `...Plot.cpp` File. Plot is an object inside a method from the main specific fidelity class class and NOT an inherited class.
+All methods for a report must be on the low level for a specific fidelity in a separate `...Plot.cpp` File. Plot is an object inside a method from the main specific fidelity class class and NOT an inherited class.
 
 !!! note
     In case `plot.h` is used: Plots which are not added to the report (not part of the map `plots`) will not appear on the generated report!
 
+### Have a closer look ...
+How different strategies are handled, have a look at other modules. If you have questions, ask the unicado team!
 
-
-
+!!! tip
+    Have a look at modules like `wing_design`, `systems_design` or `mission_analysis` as a first start.
diff --git a/docs/get-involved/modularization/python-template/cost_estimation/cost_estimation.py b/docs/get-involved/modularization/python-template/cost_estimation/cost_estimation.py
index 0a16cd5eaee48b75b3a63e6a791703045ef2f6b9..3a0d3bae96be7f2d4582bb52e7baf97e34c487a7 100644
--- a/docs/get-involved/modularization/python-template/cost_estimation/cost_estimation.py
+++ b/docs/get-involved/modularization/python-template/cost_estimation/cost_estimation.py
@@ -1,88 +1,89 @@
-"""Calculation module main file."""
-# Import standard modules.
-import logging
-import traceback
-from sys import argv, exit
-
-# Import own modules.
-from runmodule import run_module
-from src.datapreprocessing import data_preprocessing
-from src.datapostprocessing import data_postprocessing
-
-
-def main():
-    """Execute the main program for cost estimation.
-
-    This function serves as the main entry point for performing the cost estimation.
-    It goes through the following key steps:
-        (1) Preprocessing - Acquire necessary data and paths: Call the 'data_preprocessing' function from
-        'datapreprocessing.py' to set up data and routing information.
-        (2) Run (main processing) - Execute code depending on method layers: Execute the 'run_module' function from the
-        'methodexecutionpackage' library. The 'run_module' function is responsible for the programs primary logic.
-        (3) Postprocessing - Write data to the aircraft exchange file and generate plots and reports: Call the
-        'data_postprocessing' function from 'datapostprocessing.py' to handle postprocessing tasks. This step receives
-        data from both the preprocessing and the main processing step.
-
-    Note: The 'routing_dict' dictionary is used to manage the routing and execution of different program components.
-
-    :raises Exception: Raised to handle other exceptions
-    :return: None
-    """
-
-    # Initialize exception string and runtime output logger.
-    tool_name = 'cost estimation'
-    runtime_output = logging.getLogger('module_logger')
-
-    try:
-        """Preprocessing: Acquire necessary data and paths."""
-        # Run 'data_preprocessing' function from 'datapreprocessing.py'.
-        paths_and_names, routing_dict, runtime_output = data_preprocessing('cost_estimation_conf.xml', argv)
-        runtime_output.print('Cost estimation started...')
-
-        """Run: Execute code depending on method layers."""
-        # Execute 'run_module' function from 'methodexecutionpackage' library. This function is responsible for the main
-        # logic of the program.
-        run_output_dict = run_module(paths_and_names, routing_dict, runtime_output)
-
-        """Postprocessing: Write data to aircraft exchange file and generate plots and reports."""
-        # Run 'data_postprocessing' function from 'datapostprocessing.py' to handle postprocessing tasks. Receives data
-        # from preprocessing and main processing step.
-        data_postprocessing(paths_and_names, routing_dict, run_output_dict, runtime_output)
-        runtime_output.print('Operating cost estimation finished.')
-
-    except Exception as e:  # pylint: disable=broad-exception-caught
-        # Handle other exceptions.
-        runtime_output.critical(exception_string_msg(e, tool_name))
-        exit(1)
-
-
-def exception_string_msg(error, tool_name: str):
-    """Generate exception message.
-
-    Generate a formatted string detailing the type and location of an exception, along with an error message, for
-    diagnostic purposes. This function is particularly useful for logging or displaying comprehensive error information
-    when an exception occurs in a specific module or function.
-
-    :param exception error: Caught exception object from which details will be extracted
-    :param str tool_name: Name of the tool or module where the error occurred, used in the final error message
-    :return str: String including error type, file name, function/method name, line number, code that caused the error,
-    and error message.
-    """
-    error_type = str(type(error).__name__)
-    error_trace = traceback.extract_tb(error.__traceback__)
-    error_file, error_line, error_func, error_code = error_trace[-1]
-    error_file = error_file.split('/')[-1]
-
-    exception_string = f"{error_type}: \n"
-    exception_string += f"                                   - File             : {error_file} \n"
-    exception_string += f"                                   - Function / Method: {error_func} \n"
-    exception_string += f"                                   - Line             : {error_line} \n"
-    exception_string += f"                                   - Code             : {error_code} \n"
-    exception_string += f"                                   - Error message    : {str(error)} \n"
-
-    return exception_string + f"Main execution of {tool_name} module failed! \n" \
-                              f"Program aborted."
-
-
-if __name__ == "__main__":
-    main()
+"""Calculation module main file."""
+# Import standard modules.
+import logging
+import traceback
+from sys import argv, exit
+
+# Import own modules.
+from runmodule import run_module
+from src.datapreprocessing import data_preprocessing
+from src.datapostprocessing import data_postprocessing
+
+
+def main():
+    """Execute the main program for cost estimation.
+
+    This function serves as the main entry point for performing the cost estimation.
+    It goes through the following key steps:
+        (1) Preprocessing - Acquire necessary data and paths: Call the 'data_preprocessing' function from
+        'datapreprocessing.py' to set up data and routing information.
+        (2) Run (main processing) - Execute code depending on method layers: Execute the 'run_module' function from the
+        'methodexecutionpackage' library. The 'run_module' function is responsible for the programs primary logic.
+        (3) Postprocessing - Write data to the aircraft exchange file and generate plots and reports: Call the
+        'data_postprocessing' function from 'datapostprocessing.py' to handle postprocessing tasks. This step receives
+        data from both the preprocessing and the main processing step.
+
+    Note: The 'routing_dict' dictionary is used to manage the routing and execution of different program components.
+
+    :raises Exception: Raised to handle other exceptions
+    :return: None
+    """
+
+    # Initialize exception string and runtime output logger.
+    tool_name = 'cost estimation'
+    tool_version = '0.5.0'
+    runtime_output = logging.getLogger('module_logger')
+
+    try:
+        """Preprocessing: Acquire necessary data and paths."""
+        # Run 'data_preprocessing' function from 'datapreprocessing.py'.
+        paths_and_names, routing_dict, runtime_output = data_preprocessing('cost_estimation_conf.xml', tool_version, argv)
+        runtime_output.print('Cost estimation started...')
+
+        """Run: Execute code depending on method layers."""
+        # Execute 'run_module' function from 'methodexecutionpackage' library. This function is responsible for the main
+        # logic of the program.
+        run_output_dict = run_module(paths_and_names, routing_dict, runtime_output)
+
+        """Postprocessing: Write data to aircraft exchange file and generate plots and reports."""
+        # Run 'data_postprocessing' function from 'datapostprocessing.py' to handle postprocessing tasks. Receives data
+        # from preprocessing and main processing step.
+        data_postprocessing(paths_and_names, routing_dict, run_output_dict, runtime_output)
+        runtime_output.print('Operating cost estimation finished.')
+
+    except Exception as e:  # pylint: disable=broad-exception-caught
+        # Handle other exceptions.
+        runtime_output.critical(exception_string_msg(e, tool_name))
+        exit(1)
+
+
+def exception_string_msg(error, tool_name: str):
+    """Generate exception message.
+
+    Generate a formatted string detailing the type and location of an exception, along with an error message, for
+    diagnostic purposes. This function is particularly useful for logging or displaying comprehensive error information
+    when an exception occurs in a specific module or function.
+
+    :param exception error: Caught exception object from which details will be extracted
+    :param str tool_name: Name of the tool or module where the error occurred, used in the final error message
+    :return str: String including error type, file name, function/method name, line number, code that caused the error,
+    and error message.
+    """
+    error_type = str(type(error).__name__)
+    error_trace = traceback.extract_tb(error.__traceback__)
+    error_file, error_line, error_func, error_code = error_trace[-1]
+    error_file = error_file.split('/')[-1]
+
+    exception_string = f"{error_type}: \n"
+    exception_string += f"                                   - File             : {error_file} \n"
+    exception_string += f"                                   - Function / Method: {error_func} \n"
+    exception_string += f"                                   - Line             : {error_line} \n"
+    exception_string += f"                                   - Code             : {error_code} \n"
+    exception_string += f"                                   - Error message    : {str(error)} \n"
+
+    return exception_string + f"Main execution of {tool_name} module failed! \n" \
+                              f"Program aborted."
+
+
+if __name__ == "__main__":
+    main()
diff --git a/docs/get-involved/modularization/python-template/cost_estimation/cost_estimation_conf.xml b/docs/get-involved/modularization/python-template/cost_estimation/cost_estimation_conf.xml
index 5c78866a2c4abb97ee924a947ac39a642c529883..425dace73a46c18373167f6f49d0b80604767ac2 100644
--- a/docs/get-involved/modularization/python-template/cost_estimation/cost_estimation_conf.xml
+++ b/docs/get-involved/modularization/python-template/cost_estimation/cost_estimation_conf.xml
@@ -2,10 +2,10 @@
 	<module_configuration_file Name="Cost Estimation Runtime Configuration"> <!-- Change naming according to module name -->
         <control_settings description="General control settings for this tool">
             <aircraft_exchange_file_name description="Specify the name of the exchange file">
-                <value>CSR-02.xml</value>
+                <value>UNICADO-SMR-180-TF.xml</value>
             </aircraft_exchange_file_name>
             <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
-                <value>./projects/CSR/CSR-02/</value>
+                <value>../projects/UNICADO-SMR/UNICADO-SMR-180-TF/</value>
             </aircraft_exchange_file_directory>
             <own_tool_level description="Specify the tool level of this tool">
                 <value>2</value>
diff --git a/docs/get-involved/modularization/python-template/cost_estimation/src/datapreprocessing.py b/docs/get-involved/modularization/python-template/cost_estimation/src/datapreprocessing.py
index 8ac87546f3daa0f7ec18644426478d76d44d0668..f84e3b2788040af6f03a4b7c56ca9ca69e6b41be 100644
--- a/docs/get-involved/modularization/python-template/cost_estimation/src/datapreprocessing.py
+++ b/docs/get-involved/modularization/python-template/cost_estimation/src/datapreprocessing.py
@@ -1,126 +1,127 @@
-"""Module providing functions for data preprocessing."""
-# Import standard modules.
-import importlib
-import sys
-
-# Import own modules.
-from datapreprocessingmodule import get_paths_and_names, read_routing_values_from_xml
-from src.readlayertext import read_energy_carrier
-
-
-def data_preprocessing(module_configuration_file, argv):
-    """Conduct data preprocessing.
-
-    This function provides data preprocessing functionalities. It sets up the necessary data and imports relevant
-    modules. The importlib module is used to dynamically import necessary modules.
-
-    The output dictionary 'preprocessing_dict' contains the following values:
-        - 'layer_1': First routing layer (aircraft configuration) (str)
-        - 'layer_2': Second routing layer (calculation method fidelity) (str)
-        - 'layer_3': Third routing layer (calculation method) (str)
-        - 'user_layer': Last routing layer (fuel type) (user layer) (str)
-        - 'tool_level': Tool level of current tool (str)
-        - 'module_import_name': Dynamic string for dynamically generated module import name based on layers (str)
-        - 'module_name': Module name (name of the module configuration file without its file extension) (str)
-        - 'func_user_method_data_input_preparation': Reference to 'user_method_data_input_preparation' function
-        - 'func_user_method_data_output_preparation': Reference to 'user_method_data_output_preparation' function
-        - 'func_user_method_plot': Reference to 'method_plot' function
-        - 'func_user_method_html_report': Reference to 'method_html_report' function
-        - 'func_user_method_xml_export': Reference to 'method_xml_export' function
-
-    :param str module_configuration_file: Name of module configuration file
-    :param list argv: List with optional input arguments
-    :raises ModuleNotFoundError: Raised if module import failed
-    :returns:
-        - dict paths_and_names: Dictionary containing system paths and ElementTrees
-        - dict preprocessing_dict: Dictionary containing data preprocessing results
-        - logging.Logger runtime_output: Logging object used for capturing log messages in the module
-
-    """
-
-    """Get paths, names, and xml trees for module configuration and aircraft exchange file."""
-    # Call 'get_paths_and_names' function to obtain various paths and names.
-    paths_and_names, runtime_output = get_paths_and_names(module_configuration_file, argv)
-    # Note: It is the exclusive responsibility of the module manager to modify the following information!
-    # Create layer description dictionary according to the number of individual layers. The dictionary associates
-    # layers with their respective XML paths and expected data types according to the following scheme:
-    #   layer_description_dict = {'layer_1': [path, expected data type], 'layer_2': [...]}
-    # If any information cannot be directly extracted from a specific aircraft exchange file path, please write 'None'
-    # and manually add the missing value afterward.
-    aircraft_exchange_tmp_path = 'aircraft_exchange_file/requirements_and_specifications/design_specification/'
-    module_configuration_tmp_path = 'module_configuration_file/program_settings/configuration/'
-    layer_description_dict = {
-        'layer_1': [aircraft_exchange_tmp_path + 'configuration/configuration_type/value', float],
-        'layer_2': [module_configuration_tmp_path + 'fidelity_name/value', str],
-        'layer_3': [module_configuration_tmp_path + 'method_name/value', str],
-        'user_layer': [None, str]
-     }
-
-    """ Extract data from aircraft exchange and module configuration file."""
-    # Extract root and path to aircraft exchange file and write key data to aircraft exchange file.
-    root_of_aircraft_exchange_tree = paths_and_names['root_of_aircraft_exchange_tree']
-    root_of_module_configuration_file = paths_and_names['root_of_module_config_tree']
-    # Extract data from *.xml files based on the provided layer description (if no path information given ('None'),
-    # the entry has to be specified manually afterward). The result is stored in the 'preprocessing_dict' dictionary.
-    # It has the following output format (all values are strings):
-    #   dict_out = {'layer_1': value, 'layer_2': value, 'layer_3': value, 'user_layer': value, 'tool_level': value}
-    preprocessing_dict = read_routing_values_from_xml(layer_description_dict, root_of_aircraft_exchange_tree,
-                                                      root_of_module_configuration_file, runtime_output)
-    # Manual specification of missing layer values ('None' entry layer).
-    preprocessing_dict['user_layer'] = read_energy_carrier(root_of_aircraft_exchange_tree, runtime_output)
-
-    """Prepare and import modules."""
-    # Generate a dynamic import name 'module_import_name' for the selected calculation method modules based on the
-    # provided layer values according to the following scheme:
-    #   'src.[value of layer_1].[value of layer_2].[value of layer_3]'
-    module_import_name = 'src'
-    for _, value in list(preprocessing_dict.items())[:-2]:
-        module_import_name += '.' + value
-    # Create import commands by appending the python file name (incl. sub-folders, if necessary) to the generated
-    # 'module_import_name'. E.g., the import command for the module import from the 'usermethoddatapreparation.py' file
-    # is as follows:
-    #   'src.[value of layer_1].[value of layer_2].[value of layer_3].usermethoddatapreparation'
-    # The import command for the module import from the 'methodplot.py' file in the 'general' folder is as follows:
-    #   'src.[value of layer_1].[value of layer_2].[value of layer_3].general.methodplot'
-    # This step is executed for the following python files:
-    #   * 'usermethoddatapreparation.py'
-    #   * 'methodplot.py'
-    #   * 'methodhtmlreport.py'
-    #   * 'methodxmlexport.py'
-    #   * 'methodtexoutput'.py'
-    import_command_user_method_data_preparation = module_import_name + '.usermethoddatapreparation'
-    import_command_user_method_plot = module_import_name + '.general.methodplot'
-    import_command_user_method_html_report = module_import_name + '.general.methodhtmlreport'
-    import_command_user_method_xml_export = module_import_name + '.general.methodxmlexport'
-    import_command_user_method_tex_output = module_import_name + '.general.methodtexoutput'
-
-    # Add module name and tool level to the preprocessing_dict.
-    preprocessing_dict['module_import_name'] = module_import_name
-    preprocessing_dict['module_name'] = module_configuration_file[:-9]
-
-    # Dynamically import modules and functions based on the generated import commands.
-    try:
-        # Import functions from the specified modules.
-        import_user_method_data_preparation = importlib.import_module(import_command_user_method_data_preparation)
-        import_user_method_plot = importlib.import_module(import_command_user_method_plot)
-        import_user_method_html_report = importlib.import_module(import_command_user_method_html_report)
-        import_user_method_xml_export = importlib.import_module(import_command_user_method_xml_export)
-        import_user_method_tex_output = importlib.import_module(import_command_user_method_tex_output)
-        # Save the imported functions as variables in the 'preprocessing_dict' dictionary.
-        preprocessing_dict['func_user_method_data_input_preparation'] \
-            = import_user_method_data_preparation.user_method_data_input_preparation
-        preprocessing_dict['func_user_method_data_output_preparation'] \
-            = import_user_method_data_preparation.user_method_data_output_preparation
-        preprocessing_dict['func_user_method_plot'] = import_user_method_plot.method_plot
-        preprocessing_dict['func_user_method_html_report'] = import_user_method_html_report.method_html_report
-        preprocessing_dict['func_user_method_xml_export'] = import_user_method_xml_export.method_xml_export
-        preprocessing_dict['func_user_method_tex_output'] = import_user_method_tex_output.method_tex_output
-    # Exception handling for module import error.
-    except ModuleNotFoundError as module_import_error:
-        runtime_output_string = ('Error: ' + str(module_import_error) + ' found in '
-                                 + preprocessing_dict['module_name'] + '.\n'
-                                + '                                     Program aborted.')
-        runtime_output.critical(runtime_output_string)
-        sys.exit(1)
-
-    return paths_and_names, preprocessing_dict, runtime_output
+"""Module providing functions for data preprocessing."""
+# Import standard modules.
+import importlib
+import sys
+
+# Import own modules.
+from datapreprocessingmodule import get_paths_and_names, read_routing_values_from_xml
+from src.readlayertext import read_energy_carrier
+
+
+def data_preprocessing(module_configuration_file, tool_version, argv):
+    """Conduct data preprocessing.
+
+    This function provides data preprocessing functionalities. It sets up the necessary data and imports relevant
+    modules. The importlib module is used to dynamically import necessary modules.
+
+    The output dictionary 'preprocessing_dict' contains the following values:
+        - 'layer_1': First routing layer (aircraft configuration) (str)
+        - 'layer_2': Second routing layer (calculation method fidelity) (str)
+        - 'layer_3': Third routing layer (calculation method) (str)
+        - 'user_layer': Last routing layer (fuel type) (user layer) (str)
+        - 'tool_level': Tool level of current tool (str)
+        - 'module_import_name': Dynamic string for dynamically generated module import name based on layers (str)
+        - 'module_name': Module name (name of the module configuration file without its file extension) (str)
+        - 'func_user_method_data_input_preparation': Reference to 'user_method_data_input_preparation' function
+        - 'func_user_method_data_output_preparation': Reference to 'user_method_data_output_preparation' function
+        - 'func_user_method_plot': Reference to 'method_plot' function
+        - 'func_user_method_html_report': Reference to 'method_html_report' function
+        - 'func_user_method_xml_export': Reference to 'method_xml_export' function
+
+    :param str module_configuration_file: Name of module configuration file
+    :param list argv: List with optional input arguments
+    :raises ModuleNotFoundError: Raised if module import failed
+    :returns:
+        - dict paths_and_names: Dictionary containing system paths and ElementTrees
+        - dict preprocessing_dict: Dictionary containing data preprocessing results
+        - logging.Logger runtime_output: Logging object used for capturing log messages in the module
+
+    """
+
+    """Get paths, names, and xml trees for module configuration and aircraft exchange file."""
+    # Call 'get_paths_and_names' function to obtain various paths and names.
+    paths_and_names, runtime_output = get_paths_and_names(module_configuration_file, argv)
+    paths_and_names['tool_version'] = tool_version
+    # Note: It is the exclusive responsibility of the module manager to modify the following information!
+    # Create layer description dictionary according to the number of individual layers. The dictionary associates
+    # layers with their respective XML paths and expected data types according to the following scheme:
+    #   layer_description_dict = {'layer_1': [path, expected data type], 'layer_2': [...]}
+    # If any information cannot be directly extracted from a specific aircraft exchange file path, please write 'None'
+    # and manually add the missing value afterward.
+    aircraft_exchange_tmp_path = 'aircraft_exchange_file/requirements_and_specifications/design_specification/'
+    module_configuration_tmp_path = 'module_configuration_file/program_settings/configuration/'
+    layer_description_dict = {
+        'layer_1': [aircraft_exchange_tmp_path + 'configuration/configuration_type/value', float],
+        'layer_2': [module_configuration_tmp_path + 'fidelity_name/value', str],
+        'layer_3': [module_configuration_tmp_path + 'method_name/value', str],
+        'user_layer': [None, str]
+     }
+
+    """ Extract data from aircraft exchange and module configuration file."""
+    # Extract root and path to aircraft exchange file and write key data to aircraft exchange file.
+    root_of_aircraft_exchange_tree = paths_and_names['root_of_aircraft_exchange_tree']
+    root_of_module_configuration_file = paths_and_names['root_of_module_config_tree']
+    # Extract data from *.xml files based on the provided layer description (if no path information given ('None'),
+    # the entry has to be specified manually afterward). The result is stored in the 'preprocessing_dict' dictionary.
+    # It has the following output format (all values are strings):
+    #   dict_out = {'layer_1': value, 'layer_2': value, 'layer_3': value, 'user_layer': value, 'tool_level': value}
+    preprocessing_dict = read_routing_values_from_xml(layer_description_dict, root_of_aircraft_exchange_tree,
+                                                      root_of_module_configuration_file, runtime_output)
+    # Manual specification of missing layer values ('None' entry layer).
+    preprocessing_dict['user_layer'] = read_energy_carrier(root_of_aircraft_exchange_tree, runtime_output)
+
+    """Prepare and import modules."""
+    # Generate a dynamic import name 'module_import_name' for the selected calculation method modules based on the
+    # provided layer values according to the following scheme:
+    #   'src.[value of layer_1].[value of layer_2].[value of layer_3]'
+    module_import_name = 'src'
+    for _, value in list(preprocessing_dict.items())[:-2]:
+        module_import_name += '.' + value
+    # Create import commands by appending the python file name (incl. sub-folders, if necessary) to the generated
+    # 'module_import_name'. E.g., the import command for the module import from the 'usermethoddatapreparation.py' file
+    # is as follows:
+    #   'src.[value of layer_1].[value of layer_2].[value of layer_3].usermethoddatapreparation'
+    # The import command for the module import from the 'methodplot.py' file in the 'general' folder is as follows:
+    #   'src.[value of layer_1].[value of layer_2].[value of layer_3].general.methodplot'
+    # This step is executed for the following python files:
+    #   * 'usermethoddatapreparation.py'
+    #   * 'methodplot.py'
+    #   * 'methodhtmlreport.py'
+    #   * 'methodxmlexport.py'
+    #   * 'methodtexoutput'.py'
+    import_command_user_method_data_preparation = module_import_name + '.usermethoddatapreparation'
+    import_command_user_method_plot = module_import_name + '.general.methodplot'
+    import_command_user_method_html_report = module_import_name + '.general.methodhtmlreport'
+    import_command_user_method_xml_export = module_import_name + '.general.methodxmlexport'
+    import_command_user_method_tex_output = module_import_name + '.general.methodtexoutput'
+
+    # Add module name and tool level to the preprocessing_dict.
+    preprocessing_dict['module_import_name'] = module_import_name
+    preprocessing_dict['module_name'] = module_configuration_file[:-9]
+
+    # Dynamically import modules and functions based on the generated import commands.
+    try:
+        # Import functions from the specified modules.
+        import_user_method_data_preparation = importlib.import_module(import_command_user_method_data_preparation)
+        import_user_method_plot = importlib.import_module(import_command_user_method_plot)
+        import_user_method_html_report = importlib.import_module(import_command_user_method_html_report)
+        import_user_method_xml_export = importlib.import_module(import_command_user_method_xml_export)
+        import_user_method_tex_output = importlib.import_module(import_command_user_method_tex_output)
+        # Save the imported functions as variables in the 'preprocessing_dict' dictionary.
+        preprocessing_dict['func_user_method_data_input_preparation'] \
+            = import_user_method_data_preparation.user_method_data_input_preparation
+        preprocessing_dict['func_user_method_data_output_preparation'] \
+            = import_user_method_data_preparation.user_method_data_output_preparation
+        preprocessing_dict['func_user_method_plot'] = import_user_method_plot.method_plot
+        preprocessing_dict['func_user_method_html_report'] = import_user_method_html_report.method_html_report
+        preprocessing_dict['func_user_method_xml_export'] = import_user_method_xml_export.method_xml_export
+        preprocessing_dict['func_user_method_tex_output'] = import_user_method_tex_output.method_tex_output
+    # Exception handling for module import error.
+    except ModuleNotFoundError as module_import_error:
+        runtime_output_string = ('Error: ' + str(module_import_error) + ' found in '
+                                 + preprocessing_dict['module_name'] + '.\n'
+                                + '                                     Program aborted.')
+        runtime_output.critical(runtime_output_string)
+        sys.exit(1)
+
+    return paths_and_names, preprocessing_dict, runtime_output
diff --git a/docs/get-involved/modularization/python-template/projects/CSR/CSR-02/CSR-02.xml b/docs/get-involved/modularization/python-template/projects/CSR/CSR-02/CSR-02.xml
deleted file mode 100644
index 2582b9d7e14739a34111dd1a9e022bcd4e2af2b5..0000000000000000000000000000000000000000
--- a/docs/get-involved/modularization/python-template/projects/CSR/CSR-02/CSR-02.xml
+++ /dev/null
@@ -1,4832 +0,0 @@
-<aircraft_exchange_file>
-    <requirements_and_specifications description="Requirements and specifications">
-        <general description="General information on requirements and specifications">
-            <type description="Aircraft type">
-                <value>CeRAS</value>
-            </type>
-            <model description="Model - Version">
-                <value>CSR-02</value>
-            </model>
-        </general>
-        <design_specification description="Design specification">
-            <configuration description="Configuration information">
-                <configuration_type description="aircraft configuration: tube_and_wing / blended_wing_body">
-                    <value>tube_and_wing</value>
-                </configuration_type>
-                <undercarriage_definition description="Design description of the undercarriage.">
-                    <main_gear_mounting description="Mounting position of the main landing gear: wing_mounted / fuselage_mounted.">
-                        <value>wing_mounted</value>
-                    </main_gear_mounting>
-                </undercarriage_definition>
-            </configuration>
-            <propulsion description="Propulsion information">
-                <propulsor ID="0" description="Specific propulsor information">
-                    <mounting_position description="positions: under_wing_left / under_wing_right / over_wing_left / over_wing_right / on_fuselage_left / on_fuselage_right / in_fuselage_rear">
-                        <value>under_wing_left</value>
-                    </mounting_position>
-                    <energy_carrier description="Energy type: kerosene / liquid_hydrogen / battery / saf / hybrid (e.g, kerosene+liquid_hydrogen)">
-                        <value>kerosene</value>
-                    </energy_carrier>
-                    <degree_of_hybridization description="">
-                        <value>0.5</value>
-                    </degree_of_hybridization>
-                </propulsor>
-                <propulsor ID="1" description="Specific propulsor information">
-                    <mounting_position description="positions: under_wing_left / under_wing_right / over_wing_left / over_wing_right / on_fuselage_left / on_fuselage_right / in_fuselage_rear">
-                        <value>under_wing_left</value>
-                    </mounting_position>
-                    <energy_carrier description="Energy type: kerosene / liquid_hydrogen / battery / saf / hybrid (e.g, kerosene+liquid_hydrogen)">
-                        <value>kerosene</value>
-                    </energy_carrier>
-                    <degree_of_hybridization description="">
-                        <value>0.5</value>
-                    </degree_of_hybridization>
-                </propulsor>
-            </propulsion>
-        </design_specification>
-        <requirements description="Aircraft design requirements">
-            <top_level_aircraft_requirements description="Top level aircraft requirements (TLAR)">
-                <maximum_approach_speed description="Maximum allowed approach speed.">
-                    <value>71</value>
-                    <unit>m/s</unit>
-                    <lower_boundary>50</lower_boundary>
-                    <upper_boundary>90</upper_boundary>
-                </maximum_approach_speed>
-                <pavement_classification_number description="Runway pavment classification number (PCN) - limits the maximum allowed aircraft classification number of undercarriage.">
-                    <value>55</value>
-                    <unit>1</unit>
-                    <lower_boundary>5</lower_boundary>
-                    <upper_boundary>120</upper_boundary>
-                </pavement_classification_number>
-            </top_level_aircraft_requirements>
-            <additional_requirements description="Additional requirements">
-            </additional_requirements>
-        </requirements>
-        <everything_the_DOC_heart_desires>
-            <altitude_cruise>
-                <value>10058.4</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>m</unit>
-            </altitude_cruise>
-            <m_passenger>
-                <value>75</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>kg</unit>
-            </m_passenger>
-            <m_luggage>
-                <value>15.72</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>kg</unit>
-            </m_luggage>
-            <n_cabin_crew_members>
-                <value>4</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>kg</unit>
-            </n_cabin_crew_members>
-            <n_cockpit_crew_members>
-                <value>2</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>kg</unit>
-            </n_cockpit_crew_members>
-            <n_engines>
-                <value>2</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>kg</unit>
-            </n_engines>
-            <pax_per_class>
-                <value>0/0/0/12/138</value>
-                <unit>1</unit>
-            </pax_per_class>
-            <static_thrust_per_engine>
-                <value>128.855268</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>kg</unit>
-            </static_thrust_per_engine>
-            <m_takeoff_study>
-                <value>62560.48325</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>kg</unit>
-            </m_takeoff_study>
-            <mach_cruise>
-                <value>0.82</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>1</unit>
-            </mach_cruise>
-            <seat_load_factor_design>
-                <value>1.0</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>1</unit>
-            </seat_load_factor_design>
-            <seat_load_factor_study>
-                <value>0.8</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>1</unit>
-            </seat_load_factor_study>
-            <flights_per_year_design>
-                <value>1289</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>1</unit>
-            </flights_per_year_design>
-            <flights_per_year_study>
-                <value>2508</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>1</unit>
-            </flights_per_year_study>
-            <flight_time_design>
-                <value>2.83</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>1</unit>
-            </flight_time_design>
-            <flight_time_study>
-                <value>0.57</value>
-                <lower_boundary>0.0</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-                <unit>1</unit>
-            </flight_time_study>
-        </everything_the_DOC_heart_desires>
-    </requirements_and_specifications>
-    <sizing_point>
-        <wing_loading description="Maximum takeoff mass (MTOM) divided by wing area (Sref)" tool_evel="1">
-            <value>0</value>
-            <unit>"kg/m^2"</unit>
-        </wing_loading>
-        <thrust_to_weight description="Total thrust (kN) divided by maximum aircraft weight (kN)" tool_evel="1">
-            <value>0</value>
-            <lower_boundary>0.0</lower_boundary>
-            <upper_boundary>1.0</upper_boundary>
-            <unit>"1"</unit>
-        </thrust_to_weight>
-        <MTOM description="Maximum takeoff mass" tool_evel="1">
-            <value>0</value>
-            <unit>"kg"</unit>
-        </MTOM>
-        <OME description="Operating mass empty" tool_evel="1">
-            <value>0</value>
-            <unit>"kg"</unit>
-        </OME>
-    </sizing_point>
-    <component_design>
-        <mission_files description="Path and name of xml files containing the flight phase data" tool_level="0">
-            <design_mission_file description="Path and name of the design mission xml">
-                <value>0</value>
-            </design_mission_file>
-            <study_mission_file description="Path and name of the study mission xml">
-                <value>0</value>
-            </study_mission_file>
-        </mission_files>
-        <global_reference_point>
-            <reference_component description="">
-                <value />
-            </reference_component>
-            <x_position description="">
-                <value />
-                <unit />
-            </x_position>
-            <y_position description="">
-                <value />
-                <unit />
-            </y_position>
-            <z_position description="">
-                <value />
-                <unit />
-            </z_position>
-        </global_reference_point>
-        <wing description="wing component" tool_level="0">
-            <position description="position of wing (most forward position of part composition at y = 0)">
-                <x description="x position">
-                    <value>0.0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-inf</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </x>
-                <y description="y position">
-                    <value>0.0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-inf</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </y>
-                <z description="z position">
-                    <value>0.0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-inf</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </z>
-            </position>
-            <mass_properties description="mass_properties of component wing">
-                <mass description="component mass">
-                    <value>0.0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>-inf</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </mass>
-                <inertia description="component inertia refered to center of gravity">
-                    <j_xx description="inertia component in x">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xx>
-                    <j_yy description="inertia component in y">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yy>
-                    <j_zz description="inertia component in z">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zz>
-                    <j_xy description="inertia component in xy">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xy>
-                    <j_xz description="inertia component in xz">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xz>
-                    <j_yx description="inertia component in yx">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yx>
-                    <j_yz description="inertia component in yz">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yz>
-                    <j_zx description="inertia component in zx">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zx>
-                    <j_zy description="inertia component in zy">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zy>
-                </inertia>
-                <center_of_gravity description="component center of gravity with respect to global coordinate system">
-                    <x description="x component">
-                        <value>0.0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </x>
-                    <y description="y component">
-                        <value>0.0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </y>
-                    <z description="z component">
-                        <value>0.0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </z>
-                </center_of_gravity>
-            </mass_properties>
-            <specific>
-                <geometry>
-                    <aerodynamic_surface description="aerodynamic surface" ID="0">
-                        <name description="name of aerodynamic surface">
-                            <value>main_wing</value>
-                        </name>
-                        <position description="reference position in global coordinates">
-                            <x description="x position">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </x>
-                            <y description="y position">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </y>
-                            <z description="z position">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </z>
-                        </position>
-                        <parameters description="aerodynamic surface parameters">
-                            <direction description="unit vector according to global coordinate system for direction applied at position">
-                                <x description="x direction of unit vector">
-                                    <value>0.0</value>
-                                    <unit>1</unit>
-                                    <lower_boundary>-1.0</lower_boundary>
-                                    <upper_boundary>1.0</upper_boundary>
-                                </x>
-                                <y description="y direction of unit vector">
-                                    <value>1.0</value>
-                                    <unit>1</unit>
-                                    <lower_boundary>-1.0</lower_boundary>
-                                    <upper_boundary>1.0</upper_boundary>
-                                </y>
-                                <z description="z direction of unit vector">
-                                    <value>0.0</value>
-                                    <unit>1</unit>
-                                    <lower_boundary>-1.0</lower_boundary>
-                                    <upper_boundary>1.0</upper_boundary>
-                                </z>
-                            </direction>
-                            <symmetric description="symmetric to x-z plane (global) aerodynamic surface">
-                                <value>true</value>
-                            </symmetric>
-                            <sections description="sections">
-                                <section description="section" ID="0">
-                                    <chord_origin description="origin of chord (local)">
-                                        <x description="x position">
-                                            <value>0.0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </x>
-                                        <y description="y position">
-                                            <value>0.0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </y>
-                                        <z description="z position">
-                                            <value>0.0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </z>
-                                    </chord_origin>
-                                    <chord_length description="length of chord">
-                                        <value>0.0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>-inf</lower_boundary>
-                                        <upper_boundary>inf</upper_boundary>
-                                    </chord_length>
-                                    <geometric_twist description="geometric twist at leading edge">
-                                        <value>0.0</value>
-                                        <unit>rad</unit>
-                                        <lower_boundary>-</lower_boundary>
-                                        <upper_boundary />
-                                    </geometric_twist>
-                                    <profile description="profile (data normalized on chord)">
-                                        <name>
-                                            <value>naca0012</value>
-                                        </name>
-                                    </profile>
-                                </section>
-                            </sections>
-                            <spars description="spars">
-                                <spar description="front spar" ID="0">
-                                    <position description="chord relative position of control device">
-                                        <inner_position description="relative inner position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </inner_position>
-                                        <outer_position description="relative outer position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.2</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </outer_position>
-                                    </position>
-                                </spar>
-                                <spar description="rear spar" ID="1">
-                                    <position description="chord relative position of control device">
-                                        <inner_position description="relative inner position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </inner_position>
-                                        <outer_position description="relative outer position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.2</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </outer_position>
-                                    </position>
-                                </spar>
-                            </spars>
-                            <control_devices description="control devices">
-                                <control_device description="control device" ID="0">
-                                    <type>
-                                        <value>aileron</value>
-                                    </type>
-                                    <deflection description="maximum positive and negative deflection of control device">
-                                        <full_negative_deflection description="full negative deflection">
-                                            <value>-25.0</value>
-                                            <unit>deg</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </full_negative_deflection>
-                                        <full_positive_deflection description="full positive deflection">
-                                            <value>25.0</value>
-                                            <unit>deg</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </full_positive_deflection>
-                                    </deflection>
-                                    <position description="chord relative position of control device">
-                                        <inner_position description="relative inner position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.2</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </inner_position>
-                                        <outer_position description="relative outer position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.2</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </outer_position>
-                                    </position>
-                                </control_device>
-                            </control_devices>
-                        </parameters>
-                        <mass_properties description="mass_properties of aerodynamic surface">
-                            <mass description="component mass">
-                                <value>0.0</value>
-                                <unit>kg</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </mass>
-                            <inertia description="component inertia refered to center of gravity">
-                                <j_xx description="inertia component in x">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xx>
-                                <j_yy description="inertia component in y">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yy>
-                                <j_zz description="inertia component in z">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zz>
-                                <j_xy description="inertia component in xy">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xy>
-                                <j_xz description="inertia component in xz">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xz>
-                                <j_yx description="inertia component in yx">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yx>
-                                <j_yz description="inertia component in yz">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yz>
-                                <j_zx description="inertia component in zx">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zx>
-                                <j_zy description="inertia component in zy">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zy>
-                            </inertia>
-                            <center_of_gravity description="component center of gravity with respect to global coordinate system">
-                                <x description="x component">
-                                    <value>0.0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </x>
-                                <y description="y component">
-                                    <value>0.0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </y>
-                                <z description="z component">
-                                    <value>0.0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </z>
-                            </center_of_gravity>
-                        </mass_properties>
-                    </aerodynamic_surface>
-                </geometry>
-            </specific>
-        </wing>
-        <fuselage description="Geometric description of the aircraft fuselages" tool_level="0">
-            <position description="Position of the fuselages with regard to the global reference point.">
-                <x_position description="Distance in x direction with regard to the global reference point. (fuselage nose point)">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-10</lower_boundary>
-                    <upper_boundary>10</upper_boundary>
-                </x_position>
-                <y_position description="Distance in y direction with regard to the global reference point. (fuselage nose point)">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>0</upper_boundary>
-                </y_position>
-                <z_position description="Distance in z direction with regard to the global reference point. (distance to fuselage center line)">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-5</lower_boundary>
-                    <upper_boundary>5</upper_boundary>
-                </z_position>
-            </position>
-            <mass_properties description="Mass properties of the fuselages.">
-                <mass description="Mass of the total fuselages.">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </mass>
-                <inertia description="Inertia of the total fuselages with regard to the total center of gravity.">
-                    <j_xx description="Inertia of the total fuselages in x.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xx>
-                    <j_yy description="Inertia of the total fuselages in y.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yy>
-                    <j_zz description="Inertia of the total fuselages in z.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zz>
-                    <j_xy description="Inertia of the total fuselages in xy.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xy>
-                    <j_xz description="Inertia of the total fuselages in xz.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xz>
-                    <j_yx description="Inertia of the total fuselages in yx.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yx>
-                    <j_yz description="Inertia of the total fuselages in yz.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yz>
-                    <j_zx description="Inertia of the total fuselages in zx.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zx>
-                    <j_zy description="Inertia of the total fuselages in zy.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zy>
-                </inertia>
-                <center_of_gravity description="Center of gravity of the total fuselages.">
-                    <x_position description="Center of gravity in x-direction with regard to the global reference point. (total fuselage)">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>50</upper_boundary>
-                    </x_position>
-                    <y_position description="Center of gravity in y-direction with regard to the global reference point. (total fuselage)">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-5</lower_boundary>
-                        <upper_boundary>5</upper_boundary>
-                    </y_position>
-                    <z_position description="Center of gravity in z-direction with regard to the global reference point. (total fuselage)">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-5</lower_boundary>
-                        <upper_boundary>5</upper_boundary>
-                    </z_position>
-                </center_of_gravity>
-            </mass_properties>
-            <specific>
-                <geometry>
-                    <geometry_file_name>
-                        <value>geometryData/fuselage.dat</value>
-                    </geometry_file_name>
-                    <fuselage ID="0" description="Geometrical description of one entire fuselage.">
-                        <name description="Name of the fuselage.">
-                            <value>center_fuselage</value>
-                        </name>
-                        <position description="Position of one entire fuselage with regard to the global reference point.">
-                            <x_position description="Distance in x direction with regard to the global reference point. (fuselage nose point)">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-10</lower_boundary>
-                                <upper_boundary>10</upper_boundary>
-                            </x_position>
-                            <y_position description="Distance in y direction with regard to the global reference point. (fuselage nose point)">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-25</lower_boundary>
-                                <upper_boundary>25</upper_boundary>
-                            </y_position>
-                            <z_position description="Distance in z direction with regard to the global reference point. (distance to fuselage center line)">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-5</lower_boundary>
-                                <upper_boundary>5</upper_boundary>
-                            </z_position>
-                        </position>
-                        <mass_properties description="Mass properties of one entire fuselage.">
-                            <mass description="Mass of one entire fuslege.">
-                                <value>0</value>
-                                <unit>kg</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>100000</upper_boundary>
-                            </mass>
-                            <inertia description="Inertia of one entire fuselage with regard to his center of gravity.">
-                                <j_xx description="Inertia of one entire fuselage in x.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xx>
-                                <j_yy description="Inertia of one entire fuselage in y.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yy>
-                                <j_zz description="Inertia of one entire fuselage in z.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zz>
-                                <j_xy description="Inertia of one entire fuselage in xy.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xy>
-                                <j_xz description="Inertia of one entire fuselage in xz.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xz>
-                                <j_yx description="Inertia of one entire fuselage in yx.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yx>
-                                <j_yz description="Inertia of one entire fuselage in yz.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yz>
-                                <j_zx description="Inertia of one entire fuselage in zx.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zx>
-                                <j_zy description="Inertia of one entire fuselage in zy.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zy>
-                            </inertia>
-                            <center_of_gravity description="Center of gravity of one entire fuselage.">
-                                <x_position description="Center of gravity in x-direction with regard to the global reference point. (entire fuselage)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>50</upper_boundary>
-                                </x_position>
-                                <y_position description="Center of gravity in y-direction with regard to the global reference point. (entire fuselage)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-25</lower_boundary>
-                                    <upper_boundary>25</upper_boundary>
-                                </y_position>
-                                <z_position description="Center of gravity in z-direction with regard to the global reference point. (entire fuselage)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-5</lower_boundary>
-                                    <upper_boundary>5</upper_boundary>
-                                </z_position>
-                            </center_of_gravity>
-                        </mass_properties>
-                        <fuselage_sections description="Geometrical description of the fuselage sections of one entire fuselage">
-                            <section ID="0" description="Geometrical description of one fuselage section.">
-                                <name description="Name of the fuselage section.">
-                                    <value>section_1</value>
-                                </name>
-                                <origin description="Origin of fuselage section (local).">
-                                    <x_position description="Distance in x direction with regard to the global reference point.">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>-10</lower_boundary>
-                                        <upper_boundary>75</upper_boundary>
-                                    </x_position>
-                                    <y_position description="Distance in y direction with regard to the global reference point.">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>-25</lower_boundary>
-                                        <upper_boundary>25</upper_boundary>
-                                    </y_position>
-                                    <z_position description="Distance in z direction with regard to the global reference point.">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>-5</lower_boundary>
-                                        <upper_boundary>5</upper_boundary>
-                                    </z_position>
-                                </origin>
-                                <upper_hight description="Height of the upper half of the fuselage section.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>10</upper_boundary>
-                                </upper_hight>
-                                <lower_hight description="Height of the lower half of the fuselage section.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>10</upper_boundary>
-                                </lower_hight>
-                                <width description="Width of the fuselage section.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>10</upper_boundary>
-                                </width>
-                                <chord_length description="Maximum length of the fuselage section for bwb configuration.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>70</upper_boundary>
-                                </chord_length>
-                            </section>
-                        </fuselage_sections>
-                        <fuselage_accommodation>
-                            <position description="Position of the payload tubes with regard to the global reference point.">
-                                <x_position description="Distance in x direction with regard to the global reference point. (center payload tube starting point)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-10</lower_boundary>
-                                    <upper_boundary>10</upper_boundary>
-                                </x_position>
-                                <y_position description="Distance in y direction with regard to the global reference point. (center payload tube starting point)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>0</upper_boundary>
-                                </y_position>
-                                <z_position description="Distance in z direction with regard to the global reference point. (distance to fuselage center line)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-5</lower_boundary>
-                                    <upper_boundary>5</upper_boundary>
-                                </z_position>
-                            </position>
-                            <mass_properties description="Mass properties of the payload tubes of one entire fuselage.">
-                                <mass description="Mass of the payload tubes of one entire fuslege.">
-                                    <value>0</value>
-                                    <unit>kg</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>100000</upper_boundary>
-                                </mass>
-                                <center_of_gravity description="Center of gravity of the payload tubes of one entire fuselage.">
-                                    <x_position description="Center of gravity in x-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>0</lower_boundary>
-                                        <upper_boundary>50</upper_boundary>
-                                    </x_position>
-                                    <y_position description="Center of gravity in y-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>-5</lower_boundary>
-                                        <upper_boundary>5</upper_boundary>
-                                    </y_position>
-                                    <z_position description="Center of gravity in z-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>-5</lower_boundary>
-                                        <upper_boundary>5</upper_boundary>
-                                    </z_position>
-                                </center_of_gravity>
-                            </mass_properties>
-                            <number_of_payload_tubes description="Number of payload tubes of one entire fuselage.">
-                                <value>1</value>
-                                <unit>1</unit>
-                                <lower_boundary>1</lower_boundary>
-                                <upper_boundary>7</upper_boundary>
-                            </number_of_payload_tubes>
-                            <payload_tube ID="0" description="Geometrical description of one payload tube of the fuselage.">
-                                <name description="Name of the payload tube.">
-                                    <value>center_payload_tube</value>
-                                </name>
-                                <payload_tube_reference_points description="Payload tube center reference points in x, y and z-direction refered to fuselage nose point.">
-                                    <front_reference_points Desc="Reference points in the front of payload tube.">
-                                        <x_position Desc="Payload tube reference point in x-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-10</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </x_position>
-                                        <y_position Desc="Payload tube reference point in y-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </y_position>
-                                        <z_position Desc="Payload tube reference point in z-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </z_position>
-                                        <upper_z_position Desc="Upper payload tube reference point in z-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </upper_z_position>
-                                        <lower_z_position Desc="Lower payload tube reference point in z-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </lower_z_position>
-                                    </front_reference_points>
-                                    <aft_reference_points Desc="Reference points in the aft of payload tube.">
-                                        <x_position Desc="Payload tube reference point in x-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-10</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </x_position>
-                                        <y_position Desc="Payload tube reference point in y-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </y_position>
-                                        <z_position Desc="Payload tube reference point in z-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </z_position>
-                                        <upper_z_position Desc="Upper payload tube reference point in z-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </upper_z_position>
-                                        <lower_z_position Desc="Lower payload tube reference point in z-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </lower_z_position>
-                                    </aft_reference_points>
-                                </payload_tube_reference_points>
-                                <payload_tube_wall_reference_points description="Payload tube wall reference points in x, y and z-direction refered to fuselage nose point.">
-                                    <front_reference_points Desc="Wall reference points in the front of payload tube.">
-                                        <x_position Desc="Wall reference point in x-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-10</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </x_position>
-                                        <left_y_position Desc="Left wall reference point in y-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </left_y_position>
-                                        <right_y_position Desc="Right wall reference point in y-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </right_y_position>
-                                        <z_position Desc="Wall reference point in z-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </z_position>
-                                    </front_reference_points>
-                                    <aft_reference_points Desc="Wall reference points in the aft of payload tube.">
-                                        <x_position Desc="Wall reference point in x-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-10</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </x_position>
-                                        <left_y_position Desc="Left wall reference point in y-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </left_y_position>
-                                        <right_y_position Desc="Right wall reference point in y-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </right_y_position>
-                                        <z_position Desc="Wall reference point in z-direction">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </z_position>
-                                    </aft_reference_points>
-                                </payload_tube_wall_reference_points>
-                                <payload_tube_structural_wall_thickness description="Structural wall thickness of the paylaod tube.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>1</upper_boundary>
-                                </payload_tube_structural_wall_thickness>
-                                <payload_tube_water_volume description="Total water volume of one entire paylaod tube.">
-                                    <value>0</value>
-                                    <unit>m^3</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>infr</upper_boundary>
-                                </payload_tube_water_volume>
-                                <number_of_payload_decks description="Number of payload decks of one entire fuselage.">
-                                    <value>1</value>
-                                    <unit>1</unit>
-                                    <lower_boundary>1</lower_boundary>
-                                    <upper_boundary>3</upper_boundary>
-                                </number_of_payload_decks>
-                                <payload_deck ID="0" description="Geometrical description of the payload decks in one payload tube.">
-                                    <name description="Name of the payload deck.">
-                                        <value>passenger_deck</value>
-                                    </name>
-                                    <position description="Position of the payload deck with regard to the global reference point.">
-                                        <x_position description="Distance in x direction with regard to the global reference point. (payload deck starting point)">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-10</lower_boundary>
-                                            <upper_boundary>10</upper_boundary>
-                                        </x_position>
-                                        <y_position description="Distance in y direction with regard to the global reference point. (payload deck starting point)">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>0</upper_boundary>
-                                        </y_position>
-                                        <z_position description="Distance in z direction with regard to the global reference point. (distance to fuselage center line)">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-5</lower_boundary>
-                                            <upper_boundary>5</upper_boundary>
-                                        </z_position>
-                                    </position>
-                                    <mass_properties description="Mass properties of the payload deck of one entire payload tube.">
-                                        <mass description="Mass of the payload deck of one entire paylaod tube.">
-                                            <value>0</value>
-                                            <unit>kg</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>100000</upper_boundary>
-                                        </mass>
-                                        <center_of_gravity description="Center of gravity of the payload tubes of one entire fuselage.">
-                                            <x_position description="Center of gravity in x-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
-                                                <value>0</value>
-                                                <unit>m</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>50</upper_boundary>
-                                            </x_position>
-                                            <y_position description="Center of gravity in y-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
-                                                <value>0</value>
-                                                <unit>m</unit>
-                                                <lower_boundary>-5</lower_boundary>
-                                                <upper_boundary>5</upper_boundary>
-                                            </y_position>
-                                            <z_position description="Center of gravity in z-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
-                                                <value>0</value>
-                                                <unit>m</unit>
-                                                <lower_boundary>-5</lower_boundary>
-                                                <upper_boundary>5</upper_boundary>
-                                            </z_position>
-                                        </center_of_gravity>
-                                    </mass_properties>
-                                    <payload_deck_area description="Total floor area of the paylaod deck.">
-                                        <value>0</value>
-                                        <unit>m^2</unit>
-                                        <lower_boundary>0</lower_boundary>
-                                        <upper_boundary>1000</upper_boundary>
-                                    </payload_deck_area>
-                                    <payload_deck_water_volume description="Total water volume of the paylaod deck.">
-                                        <value>0</value>
-                                        <unit>m^3</unit>
-                                        <lower_boundary>0</lower_boundary>
-                                        <upper_boundary>1000</upper_boundary>
-                                    </payload_deck_water_volume>
-                                    <payload_deck_length description="Total length of the paylaod deck.">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>0</lower_boundary>
-                                        <upper_boundary>100</upper_boundary>
-                                    </payload_deck_length>
-                                    <payload_deck_height description="Maximum standing height of the paylaod deck.">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>0</lower_boundary>
-                                        <upper_boundary>3</upper_boundary>
-                                    </payload_deck_height>
-                                    <payload_deck_top_width description="Width on the top of the paylaod deck.">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>0</lower_boundary>
-                                        <upper_boundary>10</upper_boundary>
-                                    </payload_deck_top_width>
-                                    <payload_deck_bottom_width description="Width on the bottom of the paylaod deck.">
-                                        <value>0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>0</lower_boundary>
-                                        <upper_boundary>10</upper_boundary>
-                                    </payload_deck_bottom_width>
-                                    <payload_deck_required_power description="Required power of the payload deck.">
-                                        <value>0</value>
-                                        <unit>W</unit>
-                                        <lower_boundary>0</lower_boundary>
-                                        <upper_boundary>inf</upper_boundary>
-                                    </payload_deck_required_power>
-                                    <number_of_payload_deck_compartments description="Number of paylaod compartments of the payload deck.">
-                                        <value>1</value>
-                                        <unit>1</unit>
-                                        <lower_boundary>1</lower_boundary>
-                                        <upper_boundary>5</upper_boundary>
-                                    </number_of_payload_deck_compartments>
-                                    <payload_compartment ID="0" description="Geometrical description of the payload compartment of one payload deck.">
-                                        <name description="Name of the payload compartment of the payload deck.">
-                                            <value>front_compartment</value>
-                                        </name>
-                                        <position description="Position of the payload compartment with regard to the global reference point.">
-                                            <x_position description="Distance in x direction with regard to the global reference point. (payload compartment starting point)">
-                                                <value>0</value>
-                                                <unit>m</unit>
-                                                <lower_boundary>-10</lower_boundary>
-                                                <upper_boundary>100</upper_boundary>
-                                            </x_position>
-                                            <y_position description="Distance in y direction with regard to the global reference point. (payload compartment starting point)">
-                                                <value>0</value>
-                                                <unit>m</unit>
-                                                <lower_boundary>-25</lower_boundary>
-                                                <upper_boundary>25</upper_boundary>
-                                            </y_position>
-                                            <z_position description="Distance in z direction with regard to the global reference point. (distance compartment fuselage center line)">
-                                                <value>0</value>
-                                                <unit>m</unit>
-                                                <lower_boundary>-5</lower_boundary>
-                                                <upper_boundary>5</upper_boundary>
-                                            </z_position>
-                                        </position>
-                                        <payload_compartment_area description="Total floor area of the payload compartment.">
-                                            <value>0</value>
-                                            <unit>m^2</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>1000</upper_boundary>
-                                        </payload_compartment_area>
-                                        <payload_compartment_water_volume description="Total water volume of the paylaod compartment.">
-                                            <value>0</value>
-                                            <unit>m^3</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>1000</upper_boundary>
-                                        </payload_compartment_water_volume>
-                                        <payload_compartment_length description="Total length of the paylaod compartment.">
-                                            <value>0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>0</lower_boundary>
-                                            <upper_boundary>100</upper_boundary>
-                                        </payload_compartment_length>
-                                    </payload_compartment>
-                                </payload_deck>
-                            </payload_tube>
-                        </fuselage_accommodation>
-                    </fuselage>
-                </geometry>
-            </specific>
-        </fuselage>
-        <tank description="Description of aircraft tanks." tool_level="0">
-            <position description="Position of the tanks with regard to the global reference point.">
-                <x_position description="Distance between the foremost tank end and the global reference point in x-direction.">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>80</upper_boundary>
-                </x_position>
-                <y_position description="Distance between the foremost tank end and the global reference point in y-direction.">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-40</lower_boundary>
-                    <upper_boundary>40</upper_boundary>
-                </y_position>
-                <z_position description="Distance between the foremost tank end and the global reference point in z-direction.">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-5</lower_boundary>
-                    <upper_boundary>5</upper_boundary>
-                </z_position>
-            </position>
-            <mass_properties description="Mass properties of all tanks.">
-                <mass description="Total tank mass.">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>100000</upper_boundary>
-                </mass>
-                <inertia description="Inertia of all tanks with regard to the total center of gravity.">
-                    <j_xx description="Inertia of all tanks in x.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xx>
-                    <j_yy description="Inertia of all tanks in y.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yy>
-                    <j_zz description="Inertia of all tanks in z.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zz>
-                    <j_xy description="Inertia of all tanks in xy.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xy>
-                    <j_xz description="Inertia of all tanks in xz.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xz>
-                    <j_yx description="Inertia of all tanks in yx.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yx>
-                    <j_yz description="Inertia of all tanks in yz.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yz>
-                    <j_zx description="Inertia of all tanks in zx.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zx>
-                    <j_zy description="Inertia of all tanks in zy.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zy>
-                </inertia>
-                <center_of_gravity description="Center of gravity of all tanks.">
-                    <x_position description="Center of gravity in x-direction with regard to the global reference point.">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>80</upper_boundary>
-                    </x_position>
-                    <y_position description="Center of gravity in y-direction with regard to the global reference point.">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-40</lower_boundary>
-                        <upper_boundary>40</upper_boundary>
-                    </y_position>
-                    <z_position description="Center of gravity in z-direction with regard to the global reference point.">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-5</lower_boundary>
-                        <upper_boundary>5</upper_boundary>
-                    </z_position>
-                </center_of_gravity>
-            </mass_properties>
-            <specific>
-                <tank ID="0" description="Description of one tank.">
-                    <name description="Designator of the tank (right/left hand inner/outer wing tank, centre tank, trim tank, cylindrical/conical tail cone tank, ...).">
-                        <value>right hand inner wing tank</value>
-                    </name>
-                    <position description="Position of one tank with regard to the global reference point.">
-                        <x_position description="Distance between the foremost tank end of one tank and the global reference point in x-direction.">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>80</upper_boundary>
-                        </x_position>
-                        <y_position description="Distance between the foremost tank end of one tank and the global reference point in y-direction.">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-40</lower_boundary>
-                            <upper_boundary>40</upper_boundary>
-                        </y_position>
-                        <z_position description="Distance between the foremost tank end of one tank and the global reference point in z-direction.">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-5</lower_boundary>
-                            <upper_boundary>5</upper_boundary>
-                        </z_position>
-                    </position>
-                    <mass_properties description="Mass properties of one tank.">
-                        <mass description="Total dry mass of one tank.">
-                            <value>0</value>
-                            <unit>kg</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>100000</upper_boundary>
-                        </mass>
-                        <inertia description="Inertia of one tank with regard to its center of gravity.">
-                            <j_xx description="Inertia of one tank in x.">
-                                <value>0.0</value>
-                                <unit>kgm^2</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </j_xx>
-                            <j_yy description="Inertia of one tank in y.">
-                                <value>0.0</value>
-                                <unit>kgm^2</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </j_yy>
-                            <j_zz description="Inertia of one tank in z.">
-                                <value>0.0</value>
-                                <unit>kgm^2</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </j_zz>
-                            <j_xy description="Inertia of one tank in xy.">
-                                <value>0.0</value>
-                                <unit>kgm^2</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </j_xy>
-                            <j_xz description="Inertia of one tank in xz.">
-                                <value>0.0</value>
-                                <unit>kgm^2</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </j_xz>
-                            <j_yx description="Inertia of one tank in yx.">
-                                <value>0.0</value>
-                                <unit>kgm^2</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </j_yx>
-                            <j_yz description="Inertia of one tank in yz.">
-                                <value>0.0</value>
-                                <unit>kgm^2</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </j_yz>
-                            <j_zx description="Inertia of one tank in zx.">
-                                <value>0.0</value>
-                                <unit>kgm^2</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </j_zx>
-                            <j_zy description="Inertia of one tank in zy.">
-                                <value>0.0</value>
-                                <unit>kgm^2</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </j_zy>
-                        </inertia>
-                        <center_of_gravity description="Center of gravity of one tank.">
-                            <x_position description="Center of gravity in x-direction with regard to the global reference point.">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>80</upper_boundary>
-                            </x_position>
-                            <y_position description="Center of gravity in y-direction with regard to the global reference point.">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-40</lower_boundary>
-                                <upper_boundary>40</upper_boundary>
-                            </y_position>
-                            <z_position description="Center of gravity in z-direction with regard to the global reference point.">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-5</lower_boundary>
-                                <upper_boundary>5</upper_boundary>
-                            </z_position>
-                        </center_of_gravity>
-                    </mass_properties>
-                    <volume description="Total usable volume of one tank.">
-                        <value>0</value>
-                        <unit>l</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>100000</upper_boundary>
-                    </volume>
-                    <geometry description="Geometrical description of one tank.">
-                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
-                            <name description="Designator of tank cross section.">
-                                <value>first cross section</value>
-                            </name>
-                            <position description="Position of tank cross section with regard to the global reference point.">
-                                <x_position description="Distance between the tank cross section and the global reference point in x-direction.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>80</upper_boundary>
-                                </x_position>
-                                <y_position description="Distance between the tank cross section and the global reference point in y-direction.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-40</lower_boundary>
-                                    <upper_boundary>40</upper_boundary>
-                                </y_position>
-                                <z_position description="Distance between the tank cross section and the global reference point in z-direction.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-5</lower_boundary>
-                                    <upper_boundary>5</upper_boundary>
-                                </z_position>
-                            </position>
-                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
-                                <value>rectangular</value>
-                            </shape>
-                            <height description="Height of the cross section.">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>10</upper_boundary>
-                            </height>
-                            <width description="Width of the cross section.">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>10</upper_boundary>
-                            </width>
-                            <length description="Length of the cross section (if length &gt; 0: curved cross section, e.g., dashed tank endcap).">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>10</upper_boundary>
-                            </length>
-                        </cross_section>
-                    </geometry>
-                </tank>
-            </specific>
-        </tank>
-        <empennage description="empennage component" tool_level="0">
-            <position description="position of empennage (most forward position of part composition)">
-                <x description="x position">
-                    <value>0.0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-inf</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </x>
-                <y description="y position">
-                    <value>0.0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-inf</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </y>
-                <z description="z position">
-                    <value>0.0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-inf</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </z>
-            </position>
-            <mass_properties description="mass_properties of component empennage">
-                <mass description="component mass">
-                    <value>0.0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>-inf</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </mass>
-                <inertia description="component inertia refered to center of gravity">
-                    <j_xx description="inertia component in x">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xx>
-                    <j_yy description="inertia component in y">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yy>
-                    <j_zz description="inertia component in z">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zz>
-                    <j_xy description="inertia component in xy">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xy>
-                    <j_xz description="inertia component in xz">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xz>
-                    <j_yx description="inertia component in yx">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yx>
-                    <j_yz description="inertia component in yz">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yz>
-                    <j_zx description="inertia component in zx">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zx>
-                    <j_zy description="inertia component in zy">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zy>
-                </inertia>
-                <center_of_gravity description="component center of gravity with respect to global coordinate system">
-                    <x description="x component">
-                        <value>0.0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </x>
-                    <y description="y component">
-                        <value>0.0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </y>
-                    <z description="z component">
-                        <value>0.0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </z>
-                </center_of_gravity>
-            </mass_properties>
-            <specific>
-                <geometry>
-                    <aerodynamic_surface description="aerodynamic surface" ID="0">
-                        <name description="name of aerodynamic surface">
-                            <value>fin</value>
-                        </name>
-                        <position description="reference position in global coordinates">
-                            <x description="x position">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </x>
-                            <y description="y position">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </y>
-                            <z description="z position">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </z>
-                        </position>
-                        <parameters description="aerodynamic surface parameters">
-                            <direction description="unit vector according to global coordinate system for direction applied at position">
-                                <x description="x direction of unit vector">
-                                    <value>0.0</value>
-                                    <unit>1</unit>
-                                    <lower_boundary>-1.0</lower_boundary>
-                                    <upper_boundary>1.0</upper_boundary>
-                                </x>
-                                <y description="y direction of unit vector">
-                                    <value>1.0</value>
-                                    <unit>1</unit>
-                                    <lower_boundary>-1.0</lower_boundary>
-                                    <upper_boundary>1.0</upper_boundary>
-                                </y>
-                                <z description="z direction of unit vector">
-                                    <value>0.0</value>
-                                    <unit>1</unit>
-                                    <lower_boundary>-1.0</lower_boundary>
-                                    <upper_boundary>1.0</upper_boundary>
-                                </z>
-                            </direction>
-                            <symmetric description="symmetric to x-z plane (global) aerodynamic surface">
-                                <value>true</value>
-                            </symmetric>
-                            <sections description="sections">
-                                <section description="section" ID="0">
-                                    <chord_origin description="origin of chord (local)">
-                                        <x description="x position">
-                                            <value>0.0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </x>
-                                        <y description="y position">
-                                            <value>0.0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </y>
-                                        <z description="z position">
-                                            <value>0.0</value>
-                                            <unit>m</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </z>
-                                    </chord_origin>
-                                    <chord_length description="length of chord">
-                                        <value>0.0</value>
-                                        <unit>m</unit>
-                                        <lower_boundary>-inf</lower_boundary>
-                                        <upper_boundary>inf</upper_boundary>
-                                    </chord_length>
-                                    <geometric_twist description="geometric twist at leading edge">
-                                        <value>0.0</value>
-                                        <unit>rad</unit>
-                                        <lower_boundary>-</lower_boundary>
-                                        <upper_boundary />
-                                    </geometric_twist>
-                                    <profile description="profile (data normalized on chord)">
-                                        <name>
-                                            <value>naca0012</value>
-                                        </name>
-                                    </profile>
-                                </section>
-                            </sections>
-                            <spars description="spars">
-                                <spar description="front spar" ID="0">
-                                    <position description="chord relative position of control device">
-                                        <inner_position description="relative inner position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </inner_position>
-                                        <outer_position description="relative outer position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.2</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </outer_position>
-                                    </position>
-                                </spar>
-                                <spar description="rear spar" ID="1">
-                                    <position description="chord relative position of control device">
-                                        <inner_position description="relative inner position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </inner_position>
-                                        <outer_position description="relative outer position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.2</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </outer_position>
-                                    </position>
-                                </spar>
-                            </spars>
-                            <control_devices description="control devices">
-                                <control_device description="control device" ID="0">
-                                    <type>
-                                        <value>aileron</value>
-                                    </type>
-                                    <deflection description="maximum positive and negative deflection of control device">
-                                        <full_negative_deflection description="full negative deflection">
-                                            <value>-25.0</value>
-                                            <unit>deg</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </full_negative_deflection>
-                                        <full_positive_deflection description="full positive deflection">
-                                            <value>25.0</value>
-                                            <unit>deg</unit>
-                                            <lower_boundary>-inf</lower_boundary>
-                                            <upper_boundary>inf</upper_boundary>
-                                        </full_positive_deflection>
-                                    </deflection>
-                                    <position description="chord relative position of control device">
-                                        <inner_position description="relative inner position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.2</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </inner_position>
-                                        <outer_position description="relative outer position">
-                                            <spanwise description="relative spanwise position">
-                                                <value>0.2</value>
-                                                <unit>1</unit>
-                                                <lower_boundary>0</lower_boundary>
-                                                <upper_boundary>1.0</upper_boundary>
-                                            </spanwise>
-                                            <chord description="control device chord position">
-                                                <from description="relative chord position">
-                                                    <value>0.7</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </from>
-                                                <to description="relative chord position">
-                                                    <value>1.0</value>
-                                                    <unit>1</unit>
-                                                    <lower_boundary>0.0</lower_boundary>
-                                                    <upper_boundary>1.0</upper_boundary>
-                                                </to>
-                                            </chord>
-                                        </outer_position>
-                                    </position>
-                                </control_device>
-                            </control_devices>
-                        </parameters>
-                        <mass_properties description="mass_properties of aerodynamic surface">
-                            <mass description="component mass">
-                                <value>0.0</value>
-                                <unit>kg</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <upper_boundary>inf</upper_boundary>
-                            </mass>
-                            <inertia description="component inertia refered to center of gravity">
-                                <j_xx description="inertia component in x">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xx>
-                                <j_yy description="inertia component in y">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yy>
-                                <j_zz description="inertia component in z">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zz>
-                                <j_xy description="inertia component in xy">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xy>
-                                <j_xz description="inertia component in xz">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xz>
-                                <j_yx description="inertia component in yx">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yx>
-                                <j_yz description="inertia component in yz">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yz>
-                                <j_zx description="inertia component in zx">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zx>
-                                <j_zy description="inertia component in zy">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zy>
-                            </inertia>
-                            <center_of_gravity description="component center of gravity with respect to global coordinate system">
-                                <x description="x component">
-                                    <value>0.0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </x>
-                                <y description="y component">
-                                    <value>0.0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </y>
-                                <z description="z component">
-                                    <value>0.0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </z>
-                            </center_of_gravity>
-                        </mass_properties>
-                    </aerodynamic_surface>
-                </geometry>
-            </specific>
-        </empennage>
-        <landing_gear description="Geometric description of the aircraft undercarriage." tool_level="0">
-            <position description="Position of the total undercarriage arrangment with regard to the global reference point.">
-                <x_position description="Distance in x direction with regard to the global reference point. (total undercarriage arrangment)">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>50</upper_boundary>
-                </x_position>
-                <y_position description="Distance in y direction with regard to the global reference point. (total undercarriage arrangment)">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>0</upper_boundary>
-                </y_position>
-                <z_position description="Distance in z direction with regard to the global reference point. (total undercarriage arrangment)">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>-10</lower_boundary>
-                    <upper_boundary>0</upper_boundary>
-                </z_position>
-            </position>
-            <mass_properties description="Mass properties of the total undercarriage arrangment.">
-                <mass description="Mass of the total undercarriage arrangment.">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </mass>
-                <inertia description="Inertia of the total undercarriage arrangment with regard to the total center of gravity.">
-                    <j_xx description="Inertia of the total undercarriage arrangment in x.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xx>
-                    <j_yy description="Inertia of the total undercarriage arrangment in y.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yy>
-                    <j_zz description="Inertia of the total undercarriage arrangment in z.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zz>
-                    <j_xy description="Inertia of the total undercarriage arrangment in xy.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xy>
-                    <j_xz description="Inertia of the total undercarriage arrangment in xz.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_xz>
-                    <j_yx description="Inertia of the total undercarriage arrangment in yx.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yx>
-                    <j_yz description="Inertia of the total undercarriage arrangment in yz.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_yz>
-                    <j_zx description="Inertia of the total undercarriage arrangment in zx.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zx>
-                    <j_zy description="Inertia of the total undercarriage arrangment in zy.">
-                        <value>0.0</value>
-                        <unit>kgm^2</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </j_zy>
-                </inertia>
-                <center_of_gravity description="Center of gravity of the total undercarriage arrangment.">
-                    <x_position description="Center of gravity in x-direction with regard to the global reference point. (total undercarriage arrangment)">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>50</upper_boundary>
-                    </x_position>
-                    <y_position description="Center of gravity in y-direction with regard to the global reference point. (total undercarriage arrangment)">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>0</upper_boundary>
-                    </y_position>
-                    <z_position description="Center of gravity in z-direction with regard to the global reference point. (total undercarriage arrangment)">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-10</lower_boundary>
-                        <upper_boundary>0</upper_boundary>
-                    </z_position>
-                </center_of_gravity>
-            </mass_properties>
-            <specific>
-                <aircraft_classification_number description="Aircraft classification number for the total undercarriage arrangment.">
-                    <value>return_string</value>
-                </aircraft_classification_number>
-                <aircraft_classification_rating description="Aircraft classification rating for the total undercarriage arrangment.">
-                    <value>return_string</value>
-                </aircraft_classification_rating>
-                <geometry>
-                    <number_of_landing_gear_struts description="Number of installed landing gear struts.">
-                        <value>0</value>
-                        <unit>1</unit>
-                        <lower_boundary>3</lower_boundary>
-                        <upper_boundary>6</upper_boundary>
-                    </number_of_landing_gear_struts>
-                    <landing_gear_leg ID="0" description="Geometrical description of one entire landing gear leg.">
-                        <name description="Name of the landing gear leg.">
-                            <value>nose_gear</value>
-                        </name>
-                        <position description="Position of one entire landing gear leg with regard to the global reference point.">
-                            <x_position description="Distance in x direction with regard to the global reference point. (center line of the landing gear leg)">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>100</upper_boundary>
-                            </x_position>
-                            <y_position description="Distance in y direction with regard to the global reference point. (center line of the landing gear leg)">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-15</lower_boundary>
-                                <upper_boundary>15</upper_boundary>
-                            </y_position>
-                            <z_position description="Distance in z direction with regard to the global reference point. (z coordinate refers to the mounting point of the landing gear leg.)">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-10</lower_boundary>
-                                <upper_boundary>0</upper_boundary>
-                            </z_position>
-                        </position>
-                        <mass_properties description="Mass properties of one entire landing gear leg.">
-                            <mass description="Mass of one entire landing gear leg.">
-                                <value>0</value>
-                                <unit>kg</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>10000</upper_boundary>
-                            </mass>
-                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
-                                <j_xx description="Inertia of one entire landing gear leg in x.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xx>
-                                <j_yy description="Inertia of one entire landing gear leg in y.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yy>
-                                <j_zz description="Inertia of one entire landing gear leg in z.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zz>
-                                <j_xy description="Inertia of one entire landing gear leg xy.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xy>
-                                <j_xz description="Inertia of one entire landing gear leg in xz.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_xz>
-                                <j_yx description="Inertia of one entire landing gear leg in yx.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yx>
-                                <j_yz description="Inertia of one entire landing gear leg in yz.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_yz>
-                                <j_zx description="Inertia of one entire landing gear leg in zx.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zx>
-                                <j_zy description="Inertia of one entire landing gear leg in zy.">
-                                    <value>0.0</value>
-                                    <unit>kgm^2</unit>
-                                    <lower_boundary>-inf</lower_boundary>
-                                    <upper_boundary>inf</upper_boundary>
-                                </j_zy>
-                            </inertia>
-                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
-                                <x_position description="Center of gravity in x-direction with regard to the global reference point. (entire landing gear leg)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>50</upper_boundary>
-                                </x_position>
-                                <y_position description="Center of gravity in y-direction with regard to the global reference point. (entire landing gear leg)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>0</upper_boundary>
-                                </y_position>
-                                <z_position description="Center of gravity in z-direction with regard to the global reference point. (entire landing gear leg)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-10</lower_boundary>
-                                    <upper_boundary>0</upper_boundary>
-                                </z_position>
-                            </center_of_gravity>
-                        </mass_properties>
-                        <assambly_components>
-                            <strut_diameter Desc="Diameter of the landing gear strut.">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>1</upper_boundary>
-                            </strut_diameter>
-                            <strut_length Desc="Length of the landing gear strut.">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>10</upper_boundary>
-                            </strut_length>
-                            <wheel_group_position Desc="Position of wheel group of one entire landing gear leg.">
-                                <x_position description="Distance in x direction with regard to the global reference point (center line of the landing gear leg)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>100</upper_boundary>
-                                </x_position>
-                                <y_position description="Distance in y direction with regard to the global reference point (center line of the landing gear leg)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-15</lower_boundary>
-                                    <upper_boundary>15</upper_boundary>
-                                </y_position>
-                                <z_position description="Distance in z direction with regard to the global reference point (z coordinate refers to the end point of the landing gear leg.)">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>-20</lower_boundary>
-                                    <upper_boundary>0</upper_boundary>
-                                </z_position>
-                            </wheel_group_position>
-                            <number_of_axis_of_wheel_group Desc="Number of axis of the wheel group behind each other.">
-                                <value>0</value>
-                                <unit>1</unit>
-                                <lower_boundary>1</lower_boundary>
-                                <upper_boundary>10</upper_boundary>
-                            </number_of_axis_of_wheel_group>
-                            <wheel_base Desc="Distance of the foremost to the rearmost axis of the wheel group.">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>15</upper_boundary>
-                            </wheel_base>
-                            <wheel_track Desc="Distance between the outermost wheels of an axis.">
-                                <value>0</value>
-                                <unit>m</unit>
-                                <lower_boundary>0</lower_boundary>
-                                <upper_boundary>5</upper_boundary>
-                            </wheel_track>
-                            <number_of_tires_per_axis Desc="Number of tires per axis of a tire group.">
-                                <value>0</value>
-                                <unit>1</unit>
-                                <lower_boundary>1</lower_boundary>
-                                <upper_boundary>4</upper_boundary>
-                            </number_of_tires_per_axis>
-                            <tire_description Desc="Description of one tire of the wheel group">
-                                <tire_diameter Desc="Diameter of the wheel group tires.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>2</upper_boundary>
-                                </tire_diameter>
-                                <tire_width Desc="Width of the wheel group tires.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>1</upper_boundary>
-                                </tire_width>
-                                <rim_diameter Desc="Rim diameter of the wheel group tires.">
-                                    <value>0</value>
-                                    <unit>m</unit>
-                                    <lower_boundary>0</lower_boundary>
-                                    <upper_boundary>1</upper_boundary>
-                                </rim_diameter>
-                                <tire_pressure Desc="Tire pressure of the wheel group tires.">
-                                    <value>0</value>
-                                    <unit>Pa</unit>
-                                    <lower_boundary>1000000</lower_boundary>
-                                    <upper_boundary>2000000</upper_boundary>
-                                </tire_pressure>
-                                <maximum_tire_speed Desc="Maximum permissible tire speed of the wheel group tires.">
-                                    <value>0</value>
-                                    <unit>m/s</unit>
-                                    <lower_boundary>50</lower_boundary>
-                                    <upper_boundary>125</upper_boundary>
-                                </maximum_tire_speed>
-                            </tire_description>
-                        </assambly_components>
-                    </landing_gear_leg>
-                </geometry>
-            </specific>
-        </landing_gear>
-        <propulsion description="Propulsion components" ID="0" tool_level="0">
-            <position description="Reference positions of the propulsion assembly">
-                <nacelle description="Position of nacelle element in aircraft coordinate system (center of inlet)">
-                    <x description="x direction of nacelle">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>100</upper_boundary>
-                    </x>
-                    <y description="y direction of nacelle">
-                        <value>0</value>
-                        <unit>m</unit>
-                        <lower_boundary>-50</lower_boundary>
-                        <upper_boundary>50</upper_boundary>
-                    </y>
-                    <z description="z direction of nacelle">
-                        <unit>m</unit>
-                        <value>0</value>
-                        <lower_boundary>-20</lower_boundary>
-                        <upper_boundary>40</upper_boundary>
-                    </z>
-                </nacelle>
-            </position>
-            <mass_properties description="Mass properties of propulsion assembly">
-                <nacelle>
-                    <mass description="nacelle mass">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>10000</upper_boundary>
-                    </mass>
-                    <inertia description="nacelle inertia refered to its center of gravity">
-                        <j_xx description="inertia component in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia component in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia component in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia component in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia component in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia component in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia component in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia component in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia component in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="nacelle center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </nacelle>
-                <pylon>
-                    <mass description="component mass pylon">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>10000</upper_boundary>
-                    </mass>
-                    <inertia description="component inertia refered to center of gravity">
-                        <j_xx description="inertia component in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia component in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia component in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia component in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia component in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia component in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia component in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia component in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia component in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="component center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </pylon>
-                <engine>
-                    <mass description="component mass engine">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>10000</upper_boundary>
-                    </mass>
-                    <inertia description="component inertia refered to center of gravity">
-                        <j_xx description="inertia component in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia component in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia component in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia component in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia component in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia component in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia component in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia component in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia component in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="component center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </engine>
-            </mass_properties>
-            <specific description="Specific nacelle and engine properties">
-                <nacelle description="Parametric description of nacelle geometry">
-                    <incidence_angle description="Angle of incidence in reference to the aircrafts coordinate system">
-                        <unit>degree</unit>
-                        <lower_boundary>-10</lower_boundary>
-                        <upper_boundary>10</upper_boundary>
-                    </incidence_angle>
-                    <number_points description="No of points describing the section">
-                        <value>0</value>
-                    </number_points>
-                    <number_segments description="Number of segments describing the nacelle">
-                        <value>0</value>
-                    </number_segments>
-                    <inlet_segment description="Geometric desciption of the nacelle inlet segment">
-                        <segment_point_data>
-                            <value>0</value>
-                        </segment_point_data>
-                        <width_inlet description="Width of the nacelle segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </width_inlet>
-                        <height_inlet description="Height of the nacelle segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </height_inlet>
-                        <length_inlet description="Length of the nacelle segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </length_inlet>
-                    </inlet_segment>
-                    <nacelle_segment ID="0">
-                        <inner_segment_point_data>
-                            <value>0</value>
-                        </inner_segment_point_data>
-                        <outer_segment_point_data>
-                            <value>0</value>
-                        </outer_segment_point_data>
-                        <width_inner_segment description="Inner widht of nacelle segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </width_inner_segment>
-                        <width_outer_segment description="Outer widht of nacelle segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </width_outer_segment>
-                        <height_inner_segment description="Inner height of nacelle segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </height_inner_segment>
-                        <height_outer_segment description="Outer height of nacelle segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </height_outer_segment>
-                        <length_segment description="length of the nacelle segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </length_segment>
-                    </nacelle_segment>
-                    <exit_segment description="Geometric desciption of the nacelle exit segment">
-                        <segment_point_data>
-                            <value>0</value>
-                        </segment_point_data>
-                        <width_inlet description="Width of the nacelle exit segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </width_inlet>
-                        <height_inlet description="height of the nacelle exit segment">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>10</upper_boundary>
-                        </height_inlet>
-                    </exit_segment>
-                </nacelle>
-                <engine description="Parametric description of engine settings, geometry and performance">
-                    <settings description="Settings of engine model and improvment factor (from config)">
-                        <engine_model description="Name of selected engine model">
-                            <value>0.0</value>
-                        </engine_model>
-                        <fuel_flow_scale_factor description="Selected fuel flow scaling/improvement factor">
-                            <value>0.0</value>
-                            <lower_boundary>0.0</lower_boundary>
-                            <upper_boundary>1.0</upper_boundary>
-                        </fuel_flow_scale_factor>
-                        <maximum_shaft_power_extraction description="Maximum shaft power extraction of the engine for aircraft onboard systems">
-                            <value>0.0</value>
-                            <unit>W</unit>
-                            <lower_boundary>0.0</lower_boundary>
-                            <upper_boundary>3E+5</upper_boundary>
-                        </maximum_shaft_power_extraction>
-                    </settings>
-                    <turboprop_propeller_diameter description="Diameter of the propeller of the turboprop">
-                        <value>0.0</value>
-                        <unit>m</unit>
-                        <lower_boundary>1.75</lower_boundary>
-                        <lower_boundary>5.3</lower_boundary>
-                    </turboprop_propeller_diameter>
-                    <performance description="Performance specific parameter">
-                        <scale_factor description="Performance scaling factor">
-                            <value>0.0</value>
-                            <lower_boundary>0.0</lower_boundary>
-                            <upper_boundary>1.0</upper_boundary>
-                        </scale_factor>
-                        <maximum_take_off description="Performance at maximum take off condition at ISA+deltaISA (Requirements/DesignMission) with no offtakes at Mach=0.0 and altitude=0.0">
-                            <thrust>
-                                <value>0.0</value>
-                                <unit>N</unit>
-                                <lower_boundary>0.0</lower_boundary>
-                                <upper_boundary>999.0</upper_boundary>
-                            </thrust>
-                        </maximum_take_off>
-                        <maximum_continuous description="Performance at maximum continuous conditions at ISA+deltaISA (Requirements/DesignMission) with no offtakes at predefined Mach and altitude">
-                            <maximum_thrust description="Performance at maximum thrust at maximum continuous conditions">
-                                <thrust>
-                                    <value>0.0</value>
-                                    <unit>N</unit>
-                                    <lower_boundary>0.0</lower_boundary>
-                                    <upper_boundary>999.0</upper_boundary>
-                                </thrust>
-                                <thrust_specific_fuel_consumption>
-                                    <value>0.0</value>
-                                    <unit>kgs^-1N^-1</unit>
-                                    <lower_boundary>0.0</lower_boundary>
-                                    <upper_boundary>999.0</upper_boundary>
-                                </thrust_specific_fuel_consumption>
-                            </maximum_thrust>
-                            <bucket_thrust description="performance at bucket thrust at maximum continuous conditions">
-                                <thrust>
-                                    <value>0.0</value>
-                                    <unit>N</unit>
-                                    <lower_boundary>0.0</lower_boundary>
-                                    <upper_boundary>999.0</upper_boundary>
-                                </thrust>
-                                <thrust_specific_fuel_consumption>
-                                    <value>0.0</value>
-                                    <unit>kgs^-1N^-1</unit>
-                                    <lower_boundary>0.0</lower_boundary>
-                                    <upper_boundary>999.0</upper_boundary>
-                                </thrust_specific_fuel_consumption>
-                            </bucket_thrust>
-                        </maximum_continuous>
-                    </performance>
-                </engine>
-            </specific>
-        </propulsion>
-        <systems tool_level="0">
-            <position />
-            <mass_properties description="mass_properties of component systems">
-                <mass description="component mass">
-                    <systems_group description="total systems group">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </systems_group>
-                    <auxiliary_power_unit description="Airbus Chapter 30, ATA49">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </auxiliary_power_unit>
-                    <hydraulic_generation description="Airbus Chapter 31, ATA 29">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </hydraulic_generation>
-                    <hydraulic_distribution description="Airbus Chapter 32, ATA 29">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </hydraulic_distribution>
-                    <air_conditioning description="Airbus Chapter 33, ATA21">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </air_conditioning>
-                    <de_icing description="Airbus Chapter 34, ATA30">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </de_icing>
-                    <fire_protection description="Airbus Chapter 35, ATA26">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </fire_protection>
-                    <flight_controls description="Airbus Chapter 36, ATA27">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                        <roll description="aileron actuators, their installations and operation controls, Airbus Ch. 36.0">
-                            <value>0.0</value>
-                            <unit>kg</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </roll>
-                        <yaw description="rudder actuators, their installations and operation controls, Airbus Ch. 36.1">
-                            <value>0.0</value>
-                            <unit>kg</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </yaw>
-                        <pitch description="elevator actuators, their installations and operation controls, Airbus Ch. 36.2">
-                            <value>0.0</value>
-                            <unit>kg</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </pitch>
-                        <movable_horizontal_tail description="movable horizontal tail actuators, their installations and operation controls, Airbus Ch. 36.3">
-                            <value>0.0</value>
-                            <unit>kg</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </movable_horizontal_tail>
-                        <flaps description="flap actuators, their installations and operation controls, Airbus Ch. 36.4">
-                            <value>0.0</value>
-                            <unit>kg</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </flaps>
-                        <spoilers_airbrakes_liftdumpers description="spoiler actuators, their installations and operation controls, Airbus Ch. 36.5">
-                            <value>0.0</value>
-                            <unit>kg</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </spoilers_airbrakes_liftdumpers>
-                        <slats description="Mass of the slat actuators, their installations and operation controls, Airbus Ch. 36.6">
-                            <value>0.0</value>
-                            <unit>kg</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </slats>
-                        <common_installation description="flight control common installation, Airbus Ch. 36.7">
-                            <value>0.0</value>
-                            <unit>kg</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </common_installation>
-                    </flight_controls>
-                    <instruments description="Airbus Chapter 37, ATA31">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </instruments>
-                    <automatic_flight_system description="Airbus Chapter 38, ATA 22">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </automatic_flight_system>
-                    <navigation description="Airbus Chapter 39, ATA34">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </navigation>
-                    <communication description="Airbus Chapter 40, ATA23">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </communication>
-                    <electrical_generation description="Airbus Chapter 41, ATA24, generation">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </electrical_generation>
-                    <electrical_distribution description="Airbus Chapter 42, ATA24, distribution">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </electrical_distribution>
-                </mass>
-                <inertia />
-                <center_of_gravity description="component center of gravity with respect to global coordinate system">
-                    <systems_group description="total systems group">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </systems_group>
-                    <auxiliary_power_unit description="Airbus Chapter 30, ATA49">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </auxiliary_power_unit>
-                    <hydraulic_generation description="Airbus Chapter 31, ATA 29">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </hydraulic_generation>
-                    <hydraulic_distribution description="Airbus Chapter 32, ATA 29">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </hydraulic_distribution>
-                    <air_conditioning description="Airbus Chapter 33, ATA21">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </air_conditioning>
-                    <de_icing description="Airbus Chapter 34, ATA30">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </de_icing>
-                    <fire_protection description="Airbus Chapter 35, ATA26">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </fire_protection>
-                    <flight_controls description="Airbus Chapter 36, ATA27">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                        <roll description="aileron actuators, their installations and operation controls, Airbus Ch. 36.0">
-                            <x description="x component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </x>
-                            <y description="y component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </y>
-                            <z description="z component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </z>
-                        </roll>
-                        <yaw description="rudder actuators, their installations and operation controls, Airbus Ch. 36.1">
-                            <x description="x component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </x>
-                            <y description="y component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </y>
-                            <z description="z component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </z>
-                        </yaw>
-                        <pitch description="elevator actuators, their installations and operation controls, Airbus Ch. 36.2">
-                            <x description="x component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </x>
-                            <y description="y component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </y>
-                            <z description="z component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </z>
-                        </pitch>
-                        <movable_horizontal_tail description="movable horizontal tail actuators, their installations and operation controls, Airbus Ch. 36.3">
-                            <x description="x component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </x>
-                            <y description="y component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </y>
-                            <z description="z component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </z>
-                        </movable_horizontal_tail>
-                        <flaps description="flap actuators, their installations and operation controls, Airbus Ch. 36.4">
-                            <x description="x component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </x>
-                            <y description="y component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </y>
-                            <z description="z component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </z>
-                        </flaps>
-                        <spoilers_airbrakes_liftdumpers description="spoiler actuators, their installations and operation controls, Airbus Ch. 36.5">
-                            <x description="x component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </x>
-                            <y description="y component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </y>
-                            <z description="z component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </z>
-                        </spoilers_airbrakes_liftdumpers>
-                        <slats description="Mass of the slat actuators, their installations and operation controls, Airbus Ch. 36.6">
-                            <x description="x component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </x>
-                            <y description="y component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </y>
-                            <z description="z component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </z>
-                        </slats>
-                        <common_installation description="flight control common installation, Airbus Ch. 36.7">
-                            <x description="x component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </x>
-                            <y description="y component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </y>
-                            <z description="z component">
-                                <value>0.0</value>
-                                <unit>m</unit>
-                                <lower_boundary>-inf</lower_boundary>
-                                <lower_boundary>inf</lower_boundary>
-                            </z>
-                        </common_installation>
-                    </flight_controls>
-                    <instruments description="Airbus Chapter 37, ATA31">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </instruments>
-                    <automatic_flight_system description="Airbus Chapter 38, ATA 22">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </automatic_flight_system>
-                    <navigation description="Airbus Chapter 39, ATA34">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </navigation>
-                    <communication description="Airbus Chapter 40, ATA23">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </communication>
-                    <electrical_generation description="Airbus Chapter 41, ATA24, generation">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </electrical_generation>
-                    <electrical_distribution description="Airbus Chapter 42, ATA24, distribution">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <lower_boundary>inf</lower_boundary>
-                        </z>
-                    </electrical_distribution>
-                </center_of_gravity>
-            </mass_properties>
-            <specific>
-                <design_power description="design power of ATA29, ATA49, ATA70">
-                    <ATA29_hydraulic_system>
-                        <design_power description="maximum design power">
-                            <electric description="maximum demand for electrical power">
-                                <value>0</value>
-                                <unit>W</unit>
-                            </electric>
-                            <hydraulic description="maximum demand for hydraulic power">
-                                <value>0</value>
-                                <unit>W</unit>
-                            </hydraulic>
-                            <bleed_air description="maximum demand for bleed air">
-                                <value>0</value>
-                                <unit>kg/s</unit>
-                            </bleed_air>
-                        </design_power>
-                        <pressure description="nominal pressure of hydraulic system">
-                            <value>0</value>
-                            <unit>Pa</unit>
-                        </pressure>
-                    </ATA29_hydraulic_system>
-                    <ATA49_auxiliary_power_unit>
-                        <design_power description="maximum design power">
-                            <electric description="maximum demand for electrical power">
-                                <value>0</value>
-                                <unit>W</unit>
-                            </electric>
-                            <hydraulic description="maximum demand for hydraulic power">
-                                <value>0</value>
-                                <unit>W</unit>
-                            </hydraulic>
-                            <bleed_air description="maximum demand for bleed air">
-                                <value>0</value>
-                                <unit>kg/s</unit>
-                            </bleed_air>
-                        </design_power>
-                    </ATA49_auxiliary_power_unit>
-                    <ATA70_propulsion_system>
-                        <design_power description="maximum design power">
-                            <electric description="maximum demand for electrical power">
-                                <value>0</value>
-                                <unit>W</unit>
-                            </electric>
-                            <hydraulic description="maximum demand for hydraulic power">
-                                <value>0</value>
-                                <unit>W</unit>
-                            </hydraulic>
-                            <bleed_air description="maximum demand for bleed air">
-                                <value>0</value>
-                                <unit>kg/s</unit>
-                            </bleed_air>
-                        </design_power>
-                    </ATA70_propulsion_system>
-                </design_power>
-                <offtakes description="total shaft power and bleed air offtakes from sink systems">
-                    <design_mission>
-                        <average_cruise_offtakes description="average offtakes during cruise and changeFL for the design mission">
-                            <shaft_power_total description="total shaft offtakes from all sink systems">
-                                <value>0</value>
-                                <unit>W</unit>
-                            </shaft_power_total>
-                            <bleed_air_total description="total bleed air offtake from all sink systems">
-                                <value>0</value>
-                                <unit>kg/s</unit>
-                            </bleed_air_total>
-                        </average_cruise_offtakes>
-                    </design_mission>
-                    <study_mission>
-                        <average_cruise_offtakes description="average offtakes during cruise and changeFL for the study mission">
-                            <shaft_power_total description="total shaft offtakes from all sink systems">
-                                <value>0</value>
-                                <unit>W</unit>
-                            </shaft_power_total>
-                            <bleed_air_total description="total bleed air offtake from all sink systems">
-                                <value>0</value>
-                                <unit>kg/s</unit>
-                            </bleed_air_total>
-                        </average_cruise_offtakes>
-                    </study_mission>
-                </offtakes>
-            </specific>
-        </systems>
-    </component_design>
-    <analysis>
-        <masses_cg_inertia description="masses, cgs, inertias." tool_level="0">
-            <manufacturer_mass_empty description="MME">
-                <mass_properties description="manufacturer mass empty properties">
-                    <mass description="mass">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </manufacturer_mass_empty>
-            <operating_mass_empty description="OME">
-                <mass_properties description="operating mass empty properties">
-                    <mass description="mass">
-                        <value>42307.66255</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </operating_mass_empty>
-            <maximum_zero_fuel_mass description="MZFM">
-                <mass_properties description="maximum zero fuel mass properties">
-                    <mass description="mass">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </maximum_zero_fuel_mass>
-            <maximum_landing_mass description="MLM">
-                <mass_properties description="maximum landing  mass properties">
-                    <mass description="mass">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </maximum_landing_mass>
-            <maximum_takeoff_mass description="MTOM">
-                <mass_properties description="maximum landing mass properties">
-                    <mass description="mass">
-                        <value>79144.73202</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </maximum_takeoff_mass>
-            <maximum_payload_mass description="maximum payload mass">
-                <mass_properties description="maximum payload mass properties">
-                    <mass description="mass">
-                        <value>20000</value>
-                        <unit>kg</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </maximum_payload_mass>
-            <maximum_fuel_mass description="maximum fuel mass">
-                <mass_properties description="maximum fuel mass properties">
-                    <mass description="mass">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </maximum_fuel_mass>
-            <most_forward_mass description="mass for most forward cg position">
-                <mass_properties description="maximum fuel mass properties">
-                    <mass description="mass">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </most_forward_mass>
-            <most_aft_mass description="mass for most aft cg position">
-                <mass_properties description="most aft mass properties">
-                    <mass description="mass">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </most_aft_mass>
-            <design_mass description="design mass ">
-                <mass_properties description="design mass properties">
-                    <mass description="mass">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>0</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </design_mass>
-            <most_afterward_mass description="mass for most afterward cg position">
-                <mass_properties description="most afterward mass properties">
-                    <mass description="mass">
-                        <value>0.0</value>
-                        <unit>kg</unit>
-                        <lower_boundary>-inf</lower_boundary>
-                        <upper_boundary>inf</upper_boundary>
-                    </mass>
-                    <inertia description="inertia refered to center of gravity">
-                        <j_xx description="inertia in x">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xx>
-                        <j_yy description="inertia in y">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yy>
-                        <j_zz description="inertia in z">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zz>
-                        <j_xy description="inertia in xy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xy>
-                        <j_xz description="inertia in xz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_xz>
-                        <j_yx description="inertia in yx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yx>
-                        <j_yz description="inertia in yz">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_yz>
-                        <j_zx description="inertia in zx">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zx>
-                        <j_zy description="inertia in zy">
-                            <value>0.0</value>
-                            <unit>kgm^2</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </j_zy>
-                    </inertia>
-                    <center_of_gravity description="center of gravity with respect to global coordinate system">
-                        <x description="x component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </x>
-                        <y description="y component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </y>
-                        <z description="z component">
-                            <value>0.0</value>
-                            <unit>m</unit>
-                            <lower_boundary>-inf</lower_boundary>
-                            <upper_boundary>inf</upper_boundary>
-                        </z>
-                    </center_of_gravity>
-                </mass_properties>
-            </most_afterward_mass>
-        </masses_cg_inertia>
-        <aerodynamics description="Aerodynamcal analysis." level="0">
-            <reference_values>
-                <b description="Total wing span" tool_level="0">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>80</upper_boundary>
-                </b>
-                <MAC description="Mean aerodynamic chord" tool_level="0">
-                    <value>0</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>50</upper_boundary>
-                </MAC>
-                <S_ref description="Wing reference area" tool_level="0">
-                    <value>0</value>
-                    <unit>m^2</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>1000</upper_boundary>
-                </S_ref>
-            </reference_values>
-            <lift_coefficients>
-                <C_LmaxLanding description="Maximum lift coefficient in landing configuration" tool_level="0">
-                    <value>0</value>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </C_LmaxLanding>
-                <C_LmaxT-O description="Maximum lift coefficient in take off configuration" tool_level="0">
-                    <value>0</value>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </C_LmaxT-O>
-                <C_LoptimumCruise description="Lift coefficient at L/D_optimum at M_initial_cruise" tool_level="0">
-                    <value>0</value>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </C_LoptimumCruise>
-                <C_LgroundRoll description="Lift coefficient on ground for ground roll calculation" tool_level="0">
-                    <value>0</value>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </C_LgroundRoll>
-            </lift_coefficients>
-            <polar>
-                <polar_file description="Name of polar file" tool_level="0">
-                    <value>0</value>
-                </polar_file>
-                <configurations description="Number of configurations in the polar file" tool_level="0">
-                    <value>0</value>
-                </configurations>
-                <configuration description="Configuration in polar file marked with ID - name can vary" ID="1" tool_level="0">
-                    <type>Cruise</type>
-                    <value>0</value>
-                </configuration>
-                <configuration description="Configuration in polar file marked with ID - name can vary" ID="2" tool_level="0">
-                    <type>Departure</type>
-                    <value>0</value>
-                </configuration>
-                <configuration description="Configuration in polar file marked with ID - name can vary" ID="3" tool_level="0">
-                    <type>Departure</type>
-                    <value>0</value>
-                </configuration>
-                <configuration description="Configuration in polar file marked with ID - name can vary" ID="4" tool_level="0">
-                    <type>Departure</type>
-                    <value>0</value>
-                </configuration>
-                <configuration description="Configuration in polar file marked with ID - name can vary" ID="5" tool_level="0">
-                    <type>Approach</type>
-                    <value>0</value>
-                </configuration>
-                <configuration description="Configuration in polar file marked with ID - name can vary" ID="6" tool_level="0">
-                    <type>Approach</type>
-                    <value>0</value>
-                </configuration>
-                <configuration description="Configuration in polar file marked with ID - name can vary" ID="7" tool_level="0">
-                    <type>Approach</type>
-                    <value>0</value>
-                </configuration>
-            </polar>
-            <max_spoiler_factor description="Factor for maximum drag increase trough spoilers" tool_level="0">
-                <value>0</value>
-                <lower_boundary>1</lower_boundary>
-                <upper_boundary>inf</upper_boundary>
-            </max_spoiler_factor>
-        </aerodynamics>
-        <mission description="Mission data." tool_level="0">
-            <design_mission description="Data of design mission">
-                <range description="Range of design mission">
-                    <value>2500.496279</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>3000000</upper_boundary>
-                </range>
-                <block_time description="Block time of design mission: Time from break release to end of taxiing after landing">
-                    <value>0</value>
-                    <unit>s</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>126000</upper_boundary>
-                </block_time>
-                <flight_time description="Flight time of design mission">
-                    <value>0</value>
-                    <unit>s</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>12600</upper_boundary>
-                </flight_time>
-                <taxi_fuel_take_off description="Taxi fuel before takeoff in design mission">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>1000</upper_boundary>
-                </taxi_fuel_take_off>
-                <taxi_fuel_landing description="Taxi fuel after landing in design mission">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>1000</upper_boundary>
-                </taxi_fuel_landing>
-                <mission_fuel description="Total fuel loaded for design mission">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </mission_fuel>
-                <trip_fuel description="Fuel burned from takeoff to landing">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </trip_fuel>
-                <payload description="Payload of design mission">
-                    <value>17000</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </payload>
-                <number_of_pax description="Number of passengers of design mission">
-                    <value>0</value>
-                    <unit>1</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </number_of_pax>
-                <cargo_mass description="Cargo mass of design mission">
-                    <value>3392</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </cargo_mass>
-                <take_off_engine_derate Desc="Engine power demand">
-                    <value>0</value>
-                    <unit>1</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>1</upper_boundary>
-                </take_off_engine_derate>
-                <cruise_steps description="Cruise step information">
-                    <numer_of_cruise_steps description="Number of cruise steps in design mission">
-                        <value>0</value>
-                        <unit>-</unit>
-                    </numer_of_cruise_steps>
-                    <cruise_step description="Data of cruise step" ID="0">
-                        <relative_end_of_cruise_step description="End of cruise step relative to mission length">
-                            <value>0</value>
-                            <unit>-</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>1</upper_boundary>
-                        </relative_end_of_cruise_step>
-                        <altitude description="Altitude of cruise step">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>15000</upper_boundary>
-                        </altitude>
-                    </cruise_step>
-                </cruise_steps>
-                <take_off_mass description="Take off mass">
-                    <value>79144.73202</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </take_off_mass>
-            </design_mission>
-            <study_mission description="Data of study mission">
-                <range description="Range of study mission">
-                    <value>500.6435584</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>3000000</upper_boundary>
-                </range>
-                <block_time description="Block time of study mission: Time from break release to end of taxiing after landing">
-                    <value>0</value>
-                    <unit>s</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>126000</upper_boundary>
-                </block_time>
-                <flight_time description="Flight time of study mission">
-                    <value>0</value>
-                    <unit>s</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>12600</upper_boundary>
-                </flight_time>
-                <taxi_fuel_takeoff description="Taxi fuel before takeoff in study mission">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>500</upper_boundary>
-                </taxi_fuel_takeoff>
-                <taxi_fuel_landing description="Taxi fuel after landing in study mission">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>500</upper_boundary>
-                </taxi_fuel_landing>
-                <mission_fuel description="Total fuel loaded for study mission">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </mission_fuel>
-                <trip_fuel description="Fuel burned from takeoff to landing">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </trip_fuel>
-                <payload description="Payload of study mission">
-                    <value>13608</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </payload>
-                <cruise_steps description="Cruise step information">
-                    <numer_of_cruise_steps description="Number of cruise steps in study mission">
-                        <value>0</value>
-                        <unit>-</unit>
-                    </numer_of_cruise_steps>
-                    <cruise_step description="Data of cruise step" ID="0">
-                        <relative_end_of_cruise_step description="End of cruise step relative to mission length">
-                            <value>0</value>
-                            <unit>-</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>1</upper_boundary>
-                        </relative_end_of_cruise_step>
-                        <altitude description="Altitude of cruise step">
-                            <value>0</value>
-                            <unit>m</unit>
-                            <lower_boundary>0</lower_boundary>
-                            <upper_boundary>15000</upper_boundary>
-                        </altitude>
-                    </cruise_step>
-                </cruise_steps>
-                <payload description="Payload of study mission">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </payload>
-                <number_of_pax description="Number of passengers of study mission">
-                    <value>0</value>
-                    <unit>1</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </number_of_pax>
-                <cargo_mass description="Cargo mass of study mission">
-                    <value>0</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </cargo_mass>
-                <take_off_engine_derate Desc="Engine power demand">
-                    <value>0</value>
-                    <unit>1</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>1</upper_boundary>
-                </take_off_engine_derate>
-            </study_mission>
-        </mission>
-        <requirement_compliance>
-            <top_level_aircraft_requirements tool_level="0">
-                <design_take_off_field_length description="Switch indicating if take off field length can be maintained.">
-                    <value>0</value>
-                    <unit>-</unit>
-                    <checked description="Indicates if the value has been checked against the requirement.">
-                        <value>0</value>
-                        <unit>-</unit>
-                    </checked>
-                </design_take_off_field_length>
-                <design_landing_field_length description="Switch indicating if landing fiel length can be maintained.">
-                    <value>0</value>
-                    <unit>-</unit>
-                    <checked description="Indicates if the value has been checked against the requirement.">
-                        <value>0</value>
-                        <unit>-</unit>
-                    </checked>
-                </design_landing_field_length>
-                <design_approach_speed description="Switch indicating if approach speed can be maintained.">
-                    <value>0</value>
-                    <unit>-</unit>
-                    <checked description="Indicates if the value has been checked against the requirement.">
-                        <value>0</value>
-                        <unit>-</unit>
-                    </checked>
-                </design_approach_speed>
-            </top_level_aircraft_requirements>
-            <certification tool_level="0">
-                <climb_gradient_of_second_take_off_segment description="Switch if landing field length can be maintained">
-                    <value>0</value>
-                    <unit>-</unit>
-                    <checked description="Indicates if the value has been checked against the requirement.">
-                        <value>0</value>
-                        <unit>-</unit>
-                    </checked>
-                </climb_gradient_of_second_take_off_segment>
-                <climb_gradient_of_final_take_off_segment description="Switch if landing field length can be maintained">
-                    <value>0</value>
-                    <unit>-</unit>
-                    <checked description="Indicates if the value has been checked against the requirement.">
-                        <value>0</value>
-                        <unit>-</unit>
-                    </checked>
-                </climb_gradient_of_final_take_off_segment>
-                <climb_gradient_approach_one_engine_inoperative description="Switch if landing field length can be maintained">
-                    <value>0</value>
-                    <unit>-</unit>
-                    <checked description="Indicates if the value has been checked against the requirement.">
-                        <value>0</value>
-                        <unit>-</unit>
-                    </checked>
-                </climb_gradient_approach_one_engine_inoperative>
-                <climb_gradient_all_engines_operative description="Switch if landing field length can be maintained">
-                    <value>0</value>
-                    <unit>-</unit>
-                    <checked description="Indicates if the value has been checked against the requirement.">
-                        <value>0</value>
-                        <unit>-</unit>
-                    </checked>
-                </climb_gradient_all_engines_operative>
-            </certification>
-        </requirement_compliance>
-    </analysis>
-    <assessment>
-        <performance>
-            <speed tool_level="0">
-                <maximum_operating_mach_number description="Maximum operating mach number">
-                    <value>0</value>
-                    <unit>-</unit>
-                </maximum_operating_mach_number>
-                <maximum_operating_velocity description="Maximum oderating speed (maximum dynamic pressure)">
-                    <value>0</value>
-                    <unit>m/s</unit>
-                </maximum_operating_velocity>
-                <dive_mach_number description="Diving mach number">
-                    <value>0</value>
-                    <unit>-</unit>
-                </dive_mach_number>
-                <dive_velocity description="Diving speed">
-                    <value>0</value>
-                    <unit>m/s</unit>
-                </dive_velocity>
-                <one_g_stall_speed_velocity description="One g stall speed in clean configuration">
-                    <value>0</value>
-                    <unit>m/s</unit>
-                </one_g_stall_speed_velocity>
-            </speed>
-            <take_off tool_level="0">
-                <take_off_distance_normal_safety description="Takeoff distance at Sea Level for MTOM and (ISA + deltaISA)-Conditions(calculated by missionAnalysis using missionDesign.xml settings) with all engines operating (AEO)">
-                    <value>0</value>
-                    <unit>m</unit>
-                </take_off_distance_normal_safety>
-                <lift_off_speed_velocity Alt="v_lof" description="Lift-off speed in take-off configuration">
-                    <value>0</value>
-                    <unit>m/s</unit>
-                </lift_off_speed_velocity>
-                <decision_speed Alt="v_1" description="Decision speed">
-                    <value>0</value>
-                    <unit>m/s</unit>
-                </decision_speed>
-                <take_off_safety_speed Alt="v_2" description="Speed at screen height (35 ft)">
-                    <value>0</value>
-                    <unit>m/s</unit>
-                </take_off_safety_speed>
-                <final_take_off_speed Alt="v_FTO" description="Speed at final takeoff segment (1500 ft)">
-                    <value>0</value>
-                    <unit>m/s</unit>
-                </final_take_off_speed>
-                <time_to_screen_height description="Time to screen height">
-                    <value>0</value>
-                    <unit>s</unit>
-                </time_to_screen_height>
-                <climb_or_descend_segment_climb_gradient description="Climb gradient in second takeoff segment">
-                    <value>0</value>
-                    <unit>%</unit>
-                </climb_or_descend_segment_climb_gradient>
-                <final_segment_climb_gradient description="Climb gradient in final takeoff segment">
-                    <value>0</value>
-                    <unit>%</unit>
-                </final_segment_climb_gradient>
-                <balanced_field_length description="Balanced field length">
-                    <value>0</value>
-                    <unit>m</unit>
-                </balanced_field_length>
-            </take_off>
-            <landing tool_level="0">
-                <needed_runway_length description="Needed runway length with all engines operating and maximum landing mass">
-                    <value>0</value>
-                    <unit>m</unit>
-                </needed_runway_length>
-                <approach_speed description="Final approach speed in landing configuration and maximum landing mass">
-                    <value>0</value>
-                    <unit>m/s</unit>
-                </approach_speed>
-            </landing>
-            <range tool_level="0">
-                <range_max_payload_at_maximum_take_off_mass description="Range at maximum payload and fuel mass till maximum take off mass limit">
-                    <value>3246.489365</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </range_max_payload_at_maximum_take_off_mass>
-                <range_max_fuel_at_maximum_take_off_mass description="Range at full tanks and payload till maximum take off mass limit">
-                    <value>10458.54652</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </range_max_fuel_at_maximum_take_off_mass>
-                <payload_maximum_fuel_at_maximum_take_off_mass description="Payload at full tanks and payload till maximum take off mass limit">
-                    <value>4361.39852</value>
-                    <unit>kg</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </payload_maximum_fuel_at_maximum_take_off_mass>
-                <range_maximum_fuel_empty description="Range for no payload and full tanks">
-                    <value>10708.77812</value>
-                    <unit>m</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </range_maximum_fuel_empty>
-            </range>
-        </performance>
-        <average_temperature_response description="Integrated temperature change per year caused by aircraft operation divided by operating lifetime" tool_level="2">
-            <value>0</value>
-            <unit>K</unit>
-            <lower_boundary>0</lower_boundary>
-            <upper_boundary>1e-5</upper_boundary>
-        </average_temperature_response>
-        <operating_cost_estimation_tu_berlin description="Operating costs (sum of direct and indirect operating costs)" tool_level="2">
-            <direct_operating_costs description="Direct operating costs (sum of route independent and route dependent costs)">
-                <direct_operating_costs_annual description="Direct operating costs (DOC) per year">
-                    <value>30</value>
-                    <unit>EUR/y</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </direct_operating_costs_annual>
-            </direct_operating_costs>
-            <indirect_operating_costs description="Indirect operating costs (IOC)">
-                <indirect_operating_costs_annual description="Indirect operating costs (IOC) per year">
-                    <value>40</value>
-                    <unit>EUR/y</unit>
-                    <lower_boundary>0</lower_boundary>
-                    <upper_boundary>inf</upper_boundary>
-                </indirect_operating_costs_annual>
-            </indirect_operating_costs>
-        </operating_cost_estimation_tu_berlin>
-    </assessment>
-</aircraft_exchange_file>
\ No newline at end of file
diff --git a/docs/get-involved/modularization/python-template/projects/CSR/CSR-02/reporting/plots/[module name]_[name of plot].txt b/docs/get-involved/modularization/python-template/projects/CSR/CSR-02/reporting/plots/[module name]_[name of plot].txt
deleted file mode 100644
index e69de29bb2d1d6434b8b29ae775ad8c2e48c5391..0000000000000000000000000000000000000000
diff --git a/docs/get-involved/modularization/python-template/projects/CSR/CSR-02/reporting/report_xml/cost_estimation_results.xml b/docs/get-involved/modularization/python-template/projects/CSR/CSR-02/reporting/report_xml/cost_estimation_results.xml
deleted file mode 100644
index 7266cf694afa591575e928cb4b635e6740ddbdbd..0000000000000000000000000000000000000000
--- a/docs/get-involved/modularization/python-template/projects/CSR/CSR-02/reporting/report_xml/cost_estimation_results.xml
+++ /dev/null
@@ -1,46 +0,0 @@
-<module_results_file Name="Cost estimation specific outputs">
-    <general_information description="General information on module execution">
-        <workflow_version description="Version number of the current workflow">
-            <value>2.1.0</value>
-        </workflow_version>
-        <execution_date description="Execution date and time of the code">
-            <value>2024-11-18_10-48-55</value>
-        </execution_date>
-        <project_name description="Name of the current aircraft project">
-            <value>CSR-02</value>
-        </project_name>
-        <method_name description="Name of current module calculation method">
-            <value>operating_cost_estimation_tu_berlin</value>
-        </method_name>
-        <routing_layer description="Routing layer information">
-            <layer_1 description="Routing layer_1">
-                <value>tube_and_wing</value>
-            </layer_1>
-            <layer_2 description="Routing layer_2">
-                <value>empirical</value>
-            </layer_2>
-            <layer_3 description="Routing layer_3">
-                <value>operating_cost_estimation_tu_berlin</value>
-            </layer_3>
-            <user_layer description="Routing user_layer">
-                <value>kerosene</value>
-            </user_layer>
-        </routing_layer>
-    </general_information>
-    <calculation_results description="Results of calculation method">
-        <operating_cost_estimation_tu_berlin description="Empirical method to estimate the direct operating costs (DOC) and indirect operating costs (IOC) of an aircraft.">
-            <design_mission description="Cost estimation results of the design mission">
-                <direct_operating_costs description="Direct operating costs">
-                    <direct_operating_costs_per_year description="Direct operating costs per year at design point (sum of route dependent and route independent costs)">
-                        <value>30</value>
-                        <unit>EUR</unit>
-                    </direct_operating_costs_per_year>
-                </direct_operating_costs>
-                <indirect_operating_costs description="Indirect operating costs">
-                    <value>40</value>
-                    <unit>EUR</unit>
-                </indirect_operating_costs>
-            </design_mission>
-        </operating_cost_estimation_tu_berlin>
-    </calculation_results>
-</module_results_file>
\ No newline at end of file
diff --git a/docs/get-involved/modularization/python-template/projects/UNICADO-SMR/UNICADO-SMR-180-H2TF/UNICADO-SMR-180-H2TF.xml b/docs/get-involved/modularization/python-template/projects/UNICADO-SMR/UNICADO-SMR-180-H2TF/UNICADO-SMR-180-H2TF.xml
new file mode 100644
index 0000000000000000000000000000000000000000..64bdcb46bf94f61d7caf46dc13cbe6fca7c3cb75
--- /dev/null
+++ b/docs/get-involved/modularization/python-template/projects/UNICADO-SMR/UNICADO-SMR-180-H2TF/UNICADO-SMR-180-H2TF.xml
@@ -0,0 +1,9492 @@
+<aircraft_exchange_file>
+    <requirements_and_specifications description="Requirements and specifications">
+        <general description="General aircraft information">
+            <type description="Aircraft type">
+                <value>UNICADO</value>
+            </type>
+            <model description="Model - Version">
+                <value>SMR-180-TF</value>
+            </model>
+        </general>
+        <mission_files description="Name of xml files which are located in the mission_data directory and contain the flight phase data" tool_level="0">
+            <design_mission_file description="Name of the design mission xml">
+                <value>design_mission.xml</value>
+            </design_mission_file>
+            <study_mission_file description="Name of the study mission xml">
+                <value>study_mission.xml</value>
+            </study_mission_file>
+            <requirements_mission_file description="Name of the  requirements mission xml">
+                <value>requirements_mission.xml</value>
+            </requirements_mission_file>
+        </mission_files>
+        <design_specification description="Design specification">
+            <configuration description="Configuration information">
+                <configuration_type description="Aircraft configuration. Selector: tube_and_wing">
+                    <value>tube_and_wing</value>
+                </configuration_type>
+                <fuselage_definition description="Design description of the fuselage.">
+                    <fuselage_type description="Fuselage type. Selector: single_aisle / wide_body">
+                        <value>single_aisle</value>
+                    </fuselage_type>
+                    <fuselage_pressurization description="Switch to enable pressurized fuselage. Switch: true (On) / false (Off)">
+                        <value>true</value>
+                    </fuselage_pressurization>
+                </fuselage_definition>
+                <wing_definition description="Definitions for wing design">
+                    <mounting description="Wing mounting. Selector: low">
+                        <value>low</value>
+                    </mounting>
+                </wing_definition>
+                <empennage_definition description="Definitions for empennage design">
+                    <empennage_type description="Empennage type. Selector: conventional">
+                        <value>conventional</value>
+                    </empennage_type>
+                </empennage_definition>
+                <undercarriage_definition description="Design description of the undercarriage.">
+                    <main_gear_mounting description="Mounting position of the main landing gear. Selector: wing_mounted">
+                        <value>wing_mounted</value>
+                    </main_gear_mounting>
+                    <undercarriage_retractability description="Set retractability of landing gear. Selector: retractable / non_retractable">
+                        <value>retractable</value>
+                    </undercarriage_retractability>
+                </undercarriage_definition>
+                <tank_definition description="Energy tanks information">
+                    <tank ID="0" description="Inner left tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located. Selector: fuselage / wing / horizontal_stabilizer">
+                            <value>fuselage</value>
+                        </location>
+                        <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
+                            <value>tail_cone</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="1" description="Outer left tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>fuselage</value>
+                        </location>
+                        <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
+                            <value>rear</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                </tank_definition>
+                <loads description="Loads information">
+                    <design_load_factor description="Design load factor n">
+                        <maximum description="Maximum design load factor n">
+                            <value>2.5</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>4</upper_boundary>
+                        </maximum>
+                        <minimum description="Minimum design load factor n">
+                            <value>-1.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>-2.0</lower_boundary>
+                            <upper_boundary>0.0</upper_boundary>
+                        </minimum>
+                        <maneuver description="Standard maneuver load factor for e.g. flare">
+                            <value>1.1</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>2.0</upper_boundary>
+                        </maneuver>
+                    </design_load_factor>
+                </loads>
+                <aerodynamic_technologies description="Integration of aerodynamic technologies on the aircraft: Switch: false (no additional aerodynamic technologies are considered)">
+                    <value>false</value>
+                </aerodynamic_technologies>
+            </configuration>
+            <transport_task description="Define the transport task for aircraft project.">
+                <passenger_definition description="Define the masses of the passengers">
+                    <total_number_passengers description="Design number of passengers">
+                        <value>180</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1000</upper_boundary>
+                    </total_number_passengers>
+                    <mass_per_passenger description="Design mass of a single passenger WITHOUT luggage">
+                        <value>80</value>
+                        <unit>kg</unit>
+                        <lower_boundary>50</lower_boundary>
+                        <upper_boundary>200</upper_boundary>
+                    </mass_per_passenger>
+                    <luggage_mass_per_passenger description="Design mass of the luggage for a single passenger">
+                        <value>15</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>25</upper_boundary>
+                    </luggage_mass_per_passenger>
+                </passenger_definition>
+                <multi_passenger_deck_layout description="Switch to select a multi passenger deck fuselage design. Switch: false (Off)">
+                    <value>false</value>
+                    <default>false</default>
+                    <specific_number_of_passenger_decks>
+                        <value>2</value>
+                        <unit>-</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>3</upper_boundary>
+                        <default>2</default>
+                    </specific_number_of_passenger_decks>
+                </multi_passenger_deck_layout>
+                <passenger_class_definition>
+                    <class_distribution description="Relative passenger distribution for the classes: President Class/First Class/Business Class/Premium Economy/Economy. Sum must be equal to 1!">
+                        <value>0/0/0/0/1</value>
+                    </class_distribution>
+                </passenger_class_definition>
+                <cargo_definition description="Definition of cargo which does not belong to passengers">
+                    <additional_cargo_mass description="Mass of cargo which does not belong to passengers">
+                        <value>2200</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>25000</upper_boundary>
+                    </additional_cargo_mass>
+                    <cargo_density description="Density of cargo which does not belong to passengers">
+                        <value>165</value>
+                        <unit>kg/m^3</unit>
+                        <lower_boundary>150</lower_boundary>
+                        <upper_boundary>200</upper_boundary>
+                    </cargo_density>
+                </cargo_definition>
+            </transport_task>
+            <energy_carriers description="Energy carriers information">
+                <energy_carrier ID="0" description="One specific energy carrier">
+                    <type description="Energy type (for multifuel engine create new ID). Selector: kerosene">
+                        <value>liquid_hydrogen</value>
+                    </type>
+                    <density description="Energy carrier density.">
+                        <value>70.79</value>
+                        <unit>kg/m^3</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>10000</upper_boundary>
+                    </density>
+                </energy_carrier>
+            </energy_carriers>
+            <propulsion description="Propulsion information">
+                <propulsor ID="0" description="Information for specific propulsor">
+                    <powertrain description="Way the power is generated from the source. Selector: turbo">
+                        <value>turbo</value>
+                    </powertrain>
+                    <type description="Type of main thrust generator. Selector: fan">
+                        <value>fan</value>
+                    </type>
+                    <position description="Propulsor position (arrangement order acc to ID order)">
+                        <parent_component description="Position on component. Selector: wing / fuselage / empennage">
+                            <value>wing</value>
+                        </parent_component>
+                        <x description="X-position (aircraft coordinate system). Selector: front / back">
+                            <value>front</value>
+                        </x>
+                        <y description="Y-position (aircraft coordinate system). Selector: left / right">
+                            <value>left</value>
+                        </y>
+                        <z description="Z-position (aircraft coordinate system). Selector: over / mid / under / in">
+                            <value>under</value>
+                        </z>
+                    </position>
+                    <energy_carrier_ID description="See energy carrier specification node">
+                        <value>0</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </energy_carrier_ID>
+                    <thrust_share description="Share of this thrust in relation to required aircraft thrust">
+                        <value>0.5</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </thrust_share>
+                </propulsor>
+                <propulsor ID="1" description="Information for specific propulsor">
+                    <powertrain description="Way the power is generated from the source. Selector: turbo">
+                        <value>turbo</value>
+                    </powertrain>
+                    <type description="Type of main thrust generator. Selector: fan">
+                        <value>fan</value>
+                    </type>
+                    <position description="Propulsor position (arrangement order acc to ID order)">
+                        <parent_component description="Position on component. Selector: wing / fuselage / empennage">
+                            <value>wing</value>
+                        </parent_component>
+                        <x description="X-position (aircraft coordinate system). Selector: front / back">
+                            <value>front</value>
+                        </x>
+                        <y description="Y-position (aircraft coordinate system). Selector: left / right">
+                            <value>right</value>
+                        </y>
+                        <z description="Z-position (aircraft coordinate system). Selector: over / mid / under / in">
+                            <value>under</value>
+                        </z>
+                    </position>
+                    <energy_carrier_ID description="See energy carrier specification node">
+                        <value>0</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </energy_carrier_ID>
+                    <thrust_share description="Share of this thrust in relation to required aircraft thrust">
+                        <value>0.5</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </thrust_share>
+                </propulsor>
+                <energy_provider description="Source where energy is coming from per segment">
+                    <ground description="Source where energy is coming from in the ground mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </ground>
+                    <taxi description="source where energy is coming from in the taxi mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi>
+                    <takeoff description="source where energy is coming from in the takeoff mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </takeoff>
+                    <climb description="source where energy is coming from in the climb mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </climb>
+                    <cruise description="source where energy is coming from in the cruise mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </cruise>
+                    <descent description="source where energy is coming from in the descent mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </descent>
+                    <landing description="source where energy is coming from in the landing mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </landing>
+                </energy_provider>
+            </propulsion>
+            <technology>
+                <variable_camber description="Switch if variable camber is used. Switch: false (Off)">
+                    <value>false</value>
+                </variable_camber>
+            </technology>
+        </design_specification>
+        <requirements description="Aircraft design requirements">
+            <top_level_aircraft_requirements description="Top level aircraft requirements (TLAR)">
+                <maximum_structrual_payload_mass description="Maximum payload mass which can be carried by the aircraft (e.g. for short trips)">
+                    <value>19300</value>
+                    <unit>kg</unit>
+                    <lower_boundary>100</lower_boundary>
+                    <upper_boundary>150000</upper_boundary>
+                </maximum_structrual_payload_mass>
+                <takeoff_distance description="Design takeoff distance (Balanced Field Length) at Sea Level with maximum takeoff mass (MTOM) and (ISA + deltaISA)-Conditions">
+                    <value>1951</value>
+                    <unit>m</unit>
+                    <lower_boundary>600</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </takeoff_distance>
+                <landing_field_length description="Needed runway length at Sea Level with maximum landing mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)">
+                    <value>2425.67</value>
+                    <unit>m</unit>
+                    <lower_boundary>600</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </landing_field_length>
+                <icao_aerodrome_reference_code description="ICAO reference code - code_number 1-4 (field length) + code_letter A-F (wing span limits) + faa ADG code number I-VI (wing span limits + tail height limits) + Aircraft Approach Category letter  A-D">
+                    <value>3CIIIC</value>
+                </icao_aerodrome_reference_code>
+                <flight_envelope description="Maxima of design flight envelope">
+                    <maximum_operating_mach_number description="Maximum operating mach number">
+                        <value>0.82</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </maximum_operating_mach_number>
+                    <maximum_operating_velocity description="Maximum operating speed (maximum dynamic pressure)">
+                        <value>180</value>
+                        <unit>m/s</unit>
+                        <lower_boundary>50</lower_boundary>
+                        <upper_boundary>250</upper_boundary>
+                    </maximum_operating_velocity>
+                    <maximum_approach_speed description="Maximum allowed approach speed.">
+                        <value>67.65</value>
+                        <unit>m/s</unit>
+                        <lower_boundary>50</lower_boundary>
+                        <upper_boundary>90</upper_boundary>
+                    </maximum_approach_speed>
+                    <maximum_operating_altitude description="Maximum operating altitude">
+                        <value>12192</value>
+                        <unit>m</unit>
+                        <lower_boundary>4500</lower_boundary>
+                        <upper_boundary>20000</upper_boundary>
+                    </maximum_operating_altitude>
+                    <maximum_altitude_one_engine_inoperative description="Maximum operating altitude with one engine inoperative">
+                        <value>4572</value>
+                        <unit>m</unit>
+                        <lower_boundary>1500</lower_boundary>
+                        <upper_boundary>12000</upper_boundary>
+                    </maximum_altitude_one_engine_inoperative>
+                    <climb_or_descent_segment_gradient description="climb / descent segment gradient">
+                        <value>0.024</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </climb_or_descent_segment_gradient>
+                </flight_envelope>
+                <pavement_classification_number description="Runway pavement classification number (PCN) - limits the maximum allowed aircraft classification number of undercarriage">
+                    <value>55</value>
+                    <unit>1</unit>
+                    <lower_boundary>5</lower_boundary>
+                    <upper_boundary>120</upper_boundary>
+                </pavement_classification_number>
+                <design_mission description="Requirements regarding the design mission">
+                    <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
+                        <value>0</value>
+                        <unit>K</unit>
+                        <lower_boundary>-100</lower_boundary>
+                        <upper_boundary>100</upper_boundary>
+                    </delta_ISA>
+                    <range description="Target range for design mission">
+                        <value>4537400</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>20000000</upper_boundary>
+                    </range>
+                    <contingency description="Contingency fuel in percentage (reserve fuel)">
+                        <value>0.06</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>0.08</upper_boundary>
+                    </contingency>
+                    <alt_dist description="Alternate distance in m (reserve fuel)">
+                        <value>370400</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>926000</upper_boundary>
+                    </alt_dist>
+                    <loiter_time description="Loiter time in seconds (reserve fuel)">
+                        <value>1800</value>
+                        <unit>s</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>3600</upper_boundary>
+                    </loiter_time>
+                    <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise">
+                        <value>0.78</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </initial_cruise_mach_number>
+                    <initial_cruise_altitude description="Initial cruise altitude (ICA) at top of descent. May be altered during cruise">
+                        <value>10058.4</value>
+                        <unit>m</unit>
+                        <lower_boundary>1000</lower_boundary>
+                        <upper_boundary>20000</upper_boundary>
+                    </initial_cruise_altitude>
+                    <climb_speed_schedule description="Climb speed for different altitudes">
+                        <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_below_FL100>
+                        <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_above_FL100>
+                        <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
+                            <value>-0.02</value>
+                            <unit>1</unit>
+                            <lower_boundary>-0.3</lower_boundary>
+                            <upper_boundary>0.01</upper_boundary>
+                        </delta_mach_climb_cruise>
+                    </climb_speed_schedule>
+                    <descent_speed_schedule description="Descent speed for different altitudes">
+                        <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_below_FL100>
+                        <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_above_FL100>
+                    </descent_speed_schedule>
+                    <time_to_climb description="Time the aircraft takes to climb to cruise altitude">
+                        <value>2100</value>
+                        <unit>s</unit>
+                        <lower_boundary>600</lower_boundary>
+                        <upper_boundary>3600</upper_boundary>
+                    </time_to_climb>
+                    <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+                        <fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)">
+                            <value>mode_0</value>
+                        </fuel_estimation_selector>
+                    </fuel_planning>
+                </design_mission>
+                <study_mission description="Requirements regarding the study mission">
+                    <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
+                        <value>0</value>
+                        <unit>K</unit>
+                        <lower_boundary>-100</lower_boundary>
+                        <upper_boundary>100</upper_boundary>
+                    </delta_ISA>
+                    <range description="Target range for the study mission">
+                        <value>1481600</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>20000000</upper_boundary>
+                    </range>
+                    <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise">
+                        <value>0.78</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </initial_cruise_mach_number>
+                    <initial_cruise_altitude description="Initial cruise altitude at top of descent. May be altered during cruise">
+                        <value>10668</value>
+                        <unit>m</unit>
+                        <lower_boundary>1000</lower_boundary>
+                        <upper_boundary>20000</upper_boundary>
+                    </initial_cruise_altitude>
+                    <climb_speed_schedule description="Climb speed for different altitudes">
+                        <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_below_FL100>
+                        <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_above_FL100>
+                        <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
+                            <value>-0.02</value>
+                            <unit>1</unit>
+                            <lower_boundary>-0.3</lower_boundary>
+                            <upper_boundary>0.01</upper_boundary>
+                        </delta_mach_climb_cruise>
+                    </climb_speed_schedule>
+                    <descent_speed_schedule description="Descent speed for different altitudes">
+                        <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_below_FL100>
+                        <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_above_FL100>
+                    </descent_speed_schedule>
+                    <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+                        <fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)">
+                            <value>mode_0</value>
+                        </fuel_estimation_selector>
+                    </fuel_planning>
+                    <payload_fractions description="Set the fraction of different design payload values for the study mission">
+                        <cargo_fraction description="Fraction of the design cargo mass which is used for the study mission">
+                            <value>0.75</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </cargo_fraction>
+                        <passenger_mass_fraction description="Fraction of the design passenger mass which is used for the study mission">
+                            <value>0.75</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </passenger_mass_fraction>
+                    </payload_fractions>
+                </study_mission>
+            </top_level_aircraft_requirements>
+            <additional_requirements description="Additional requirements">
+                <landing_gear description="Landing gear requirements and operational conditions">
+                    <friction_coefficient description="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">
+                        <value>0.03</value>
+                        <default>0.03</default>
+                        <unit>1</unit>
+                        <lower_boundary>0.02</lower_boundary>
+                        <upper_boundary>0.08</upper_boundary>
+                    </friction_coefficient>
+                    <braking_coefficient description="Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189">
+                        <value>0.34189</value>
+                        <default>0.34189</default>
+                        <unit>1</unit>
+                        <lower_boundary>0.06</lower_boundary>
+                        <upper_boundary>0.5</upper_boundary>
+                    </braking_coefficient>
+                </landing_gear>
+            </additional_requirements>
+        </requirements>
+        <assessment_scenario description="Scenario for ecological and economical assessment">
+            <flights_per_year description="Number of flights per year">
+                <value>2227</value>
+                <unit>1</unit>
+                <lower_boundary>0</lower_boundary>
+                <upper_boundary>4000</upper_boundary>
+            </flights_per_year>
+            <duration_operation description="Operating years of aircraft">
+                <value>25</value>
+                <unit>a</unit>
+                <lower_boundary>0</lower_boundary>
+                <upper_boundary>50</upper_boundary>
+            </duration_operation>
+        </assessment_scenario>
+    </requirements_and_specifications>
+    <analysis>
+        <masses_cg_inertia description="Masses, Center of Gravity, Inertias." tool_level="3">
+            <maximum_takeoff_mass description="MTOM">
+                <mass_properties description="maximum takeoff mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1452317.8298</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>5883140.3113</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>6648774.9188</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>21.5717</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.5183</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>75000.4477</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_takeoff_mass>
+            <operating_mass_empty description="OME">
+                <mass_properties description="operating mass empty properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>970318.8048</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3930628.3776</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>4442162.1769</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>19.9824</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.687</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>50109.1037</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </operating_mass_empty>
+            <manufacturer_mass_empty description="MME">
+                <mass_properties description="manufacturer mass empty properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>890205.4692</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3606100.2443</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>4075399.8019</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>19.9343</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.7488</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>45971.8991</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </manufacturer_mass_empty>
+            <maximum_zero_fuel_mass description="MZFM">
+                <mass_properties description="maximum zero fuel mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1344046.3619</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>5444547.4464</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>6153103.3751</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>20.4427</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.5631</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>69409.1037</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_zero_fuel_mass>
+            <maximum_payload_mass description="">
+                <mass_properties description="maximum payload mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>21.6379</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.2413</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>19300</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_payload_mass>
+            <maximum_landing_mass description="MLM">
+                <mass_properties description="maximum landing mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1229364.0985</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>4979985.3288</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>5628082.9282</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>19.9824</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.687</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>63486.6941</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_landing_mass>
+            <maximum_fuel_mass description="">
+                <mass_properties description="maximum fuel mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>35.5725</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0365</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>5651.1479</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_fuel_mass>
+            <ferry_range_mass description="">
+                <mass_properties description="ferry range mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>21.5624</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.6137</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>55760.2516</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </ferry_range_mass>
+            <most_forward_mass description="">
+                <mass_properties description="most forward mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>970318.8048</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3930628.3776</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>4442162.1769</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>19.4898</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>70489.3705</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </most_forward_mass>
+            <most_afterward_mass description="">
+                <mass_properties description="most afterward mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>970318.8048</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3930628.3776</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>4442162.1769</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>21.7832</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>60020.4477</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </most_afterward_mass>
+            <design_mass description="">
+                <mass_properties description="design mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1452317.8298</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>5883140.3113</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>6648774.9188</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>21.5717</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.5183</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>75000.4477</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </design_mass>
+            <design_fuel_mass description="">
+                <mass_properties description="design fuel mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>35.5866</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0369</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>5591.344</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </design_fuel_mass>
+        </masses_cg_inertia>
+        <aerodynamics description="Aerodynamical analysis" tool_level="3">
+            <polar>
+                <polar_file description="Name of polar file">
+                    <value>SMR-180-TF_design_trimmed_polar.xml</value>
+                </polar_file>
+                <configurations description="Number of configurations in the polar file">
+                    <value>7</value>
+                    <unit>1</unit>
+                    <lower_boundary>-2147483648</lower_boundary>
+                    <upper_boundary>2147483647</upper_boundary>
+                </configurations>
+                <configuration ID="0" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>cruise</value>
+                    </type>
+                    <name description=" Name">
+                        <value>clean</value>
+                    </name>
+                </configuration>
+                <configuration ID="1" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>departure</value>
+                    </type>
+                    <name description=" Name">
+                        <value>takeoff</value>
+                    </name>
+                </configuration>
+                <configuration ID="2" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>departure</value>
+                    </type>
+                    <name description=" Name">
+                        <value>takeoff_landing_gear_retracted</value>
+                    </name>
+                </configuration>
+                <configuration ID="3" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>departure</value>
+                    </type>
+                    <name description=" Name">
+                        <value>climb</value>
+                    </name>
+                </configuration>
+                <configuration ID="4" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>approach</value>
+                    </type>
+                    <name description=" Name">
+                        <value>approach</value>
+                    </name>
+                </configuration>
+                <configuration ID="5" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>approach</value>
+                    </type>
+                    <name description=" Name">
+                        <value>approach_landing_gear_out</value>
+                    </name>
+                </configuration>
+                <configuration ID="6" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>approach</value>
+                    </type>
+                    <name description=" Name">
+                        <value>landing</value>
+                    </name>
+                </configuration>
+            </polar>
+            <reference_values>
+                <b description="Wing half span">
+                    <value>35.68224296</value>
+                    <unit>m</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </b>
+                <MAC description="Mean aerodynamic chord">
+                    <value>4.488507864</value>
+                    <unit>m</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </MAC>
+                <S_ref description="Wing reference area">
+                    <value>134.0234172</value>
+                    <unit>m^2</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </S_ref>
+                <neutral_point>
+                    <x description="x component of neutral point">
+                        <value>22.70357943</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </x>
+                </neutral_point>
+            </reference_values>
+            <lift_coefficients>
+                <C_LoptimumCruise description="C_LoptimumCruise">
+                    <value>0.632</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LoptimumCruise>
+                <C_LmaxLanding description="C_LmaxLanding">
+                    <value>3.136</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LmaxLanding>
+                <C_LmaxT-O description="C_LmaxTO">
+                    <value>2.681</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LmaxT-O>
+                <C_LgroundRoll description="C_LgroundRoll">
+                    <value>0.4</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LgroundRoll>
+            </lift_coefficients>
+            <max_spoiler_factor description="max_spoiler_factor">
+                <value>2.5</value>
+                <unit>1</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </max_spoiler_factor>
+        </aerodynamics>
+        <mission description="Mission data" tool_level="0">
+            <design_mission description="Data of design mission">
+                <range description="Traveled range from break release to end of taxi at destination">
+                    <value>4538384.063</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>20000000</upper_boundary>
+                </range>
+                <loaded_mission_energy description="Amount of energy loaded into tanks (including reserves) for the mission">
+                    <mission_energy ID="0" description="Amount of energy loaded into tanks (including reserves) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>6.783426413e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </mission_energy>
+                </loaded_mission_energy>
+                <in_flight_energy description="Amount of energy needed for in-flight segments (all segments from takeoff to landing)">
+                    <trip_energy ID="0" description="Amount of energy needed for trip segments (all segments from takeoff to landing) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>5.41329264e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </trip_energy>
+                    <takeoff_energy ID="0" description="Amount of energy needed for takeoff segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>9026058430</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </takeoff_energy>
+                    <landing_energy ID="0" description="Amount of energy needed for landing segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7288548612</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </landing_energy>
+                </in_flight_energy>
+                <taxi_energy description="Amount of energy needed for taxiing specified energy carrier">
+                    <taxi_out_energy ID="0" description="Amount of energy needed for taxiing at origin for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7381362017</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_out_energy>
+                    <taxi_in_energy ID="0" description="Amount of energy needed for taxiing at destination for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>4100756676</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_in_energy>
+                </taxi_energy>
+                <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
+                    <value>21017.79804</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>45000</upper_boundary>
+                </block_time>
+                <flight_time description="Flight time for the whole mission">
+                    <value>20177.79804</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>44500</upper_boundary>
+                </flight_time>
+                <takeoff_engine_derate description="Engine power demand">
+                    <value>1</value>
+                    <unit>1</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1</upper_boundary>
+                </takeoff_engine_derate>
+                <cruise description="Characteristics of the cruise segment">
+                    <average_lift_coefficient description="Lift coefficient CL_average: Arithmetic mean over the entire cruise flight">
+                        <value>0.497905048</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </average_lift_coefficient>
+                    <minimum_lift_coefficient description="Minimum cruise flight lift coefficient CL_min">
+                        <value>0.4751027938</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </minimum_lift_coefficient>
+                    <maximum_lift_coefficient description="Maximum cruise flight lift coefficient CL_max">
+                        <value>0.5212589617</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </maximum_lift_coefficient>
+                    <top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
+                        <value>74418.20047</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_climb_mass>
+                    <top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
+                        <value>70543.5885</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_descent_mass>
+                    <top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
+                        <value>204794.9501</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>4537400</upper_boundary>
+                    </top_of_climb_range>
+                    <top_of_descent_range description="Flown range from takeoff to top of descent">
+                        <value>4323225.176</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>4537400</upper_boundary>
+                    </top_of_descent_range>
+                    <cruise_steps description="Cruise step information">
+                        <cruise_step ID="0" description="Data of a cruise step">
+                            <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+                                <value>0.4998879854</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </relative_end_of_cruise_step>
+                            <altitude description="Altitude of cruise step">
+                                <value>10058.40002</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>15000</upper_boundary>
+                            </altitude>
+                        </cruise_step>
+                        <cruise_step ID="1" description="Data of a cruise step">
+                            <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </relative_end_of_cruise_step>
+                            <altitude description="Altitude of cruise step">
+                                <value>10668.00002</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>15000</upper_boundary>
+                            </altitude>
+                        </cruise_step>
+                    </cruise_steps>
+                </cruise>
+            </design_mission>
+            <study_mission description="Data of study mission">
+                <takeoff_mass description="Takeoff mass">
+                    <value>67053.2029</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>300000</upper_boundary>
+                </takeoff_mass>
+                <range description="Traveled range from break release to end of taxi at destination">
+                    <value>1482595.498</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>20000000</upper_boundary>
+                </range>
+                <loaded_mission_energy description="Amount of energy loaded into tanks (including reserves) for the mission">
+                    <mission_energy ID="0" description="Amount of energy loaded into tanks (including reserves) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>3.034939615e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </mission_energy>
+                </loaded_mission_energy>
+                <in_flight_energy description="Amount of energy needed for in-flight segments (all segments from takeoff to landing)">
+                    <trip_energy ID="0" description="Amount of energy needed for trip segments (all segments from takeoff to landing) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>1.796191547e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </trip_energy>
+                    <takeoff_energy ID="0" description="Amount of energy needed for takeoff segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7717278972</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </takeoff_energy>
+                    <landing_energy ID="0" description="Amount of energy needed for landing segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>6881012278</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </landing_energy>
+                </in_flight_energy>
+                <taxi_energy description="Amount of energy needed for taxiing specified energy carrier">
+                    <taxi_out_energy ID="0" description="Amount of energy needed for taxiing at origin for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7202057977</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_out_energy>
+                    <taxi_in_energy ID="0" description="Amount of energy needed for taxiing at destination for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>4001143321</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_in_energy>
+                </taxi_energy>
+                <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
+                    <value>7856.162369</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>45000</upper_boundary>
+                </block_time>
+                <flight_time description="Flight time for the whole mission">
+                    <value>7016.162369</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>44500</upper_boundary>
+                </flight_time>
+                <takeoff_engine_derate description="Engine power demand">
+                    <value>1</value>
+                    <unit>1</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1</upper_boundary>
+                </takeoff_engine_derate>
+                <cruise description="Characteristics of the cruise segment">
+                    <average_lift_coefficient description="Lift coefficient CL_average: Arithmetic mean over the entire cruise flight">
+                        <value>0.4761674741</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </average_lift_coefficient>
+                    <minimum_lift_coefficient description="Minimum cruise flight lift coefficient CL_min">
+                        <value>0.4728031554</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </minimum_lift_coefficient>
+                    <maximum_lift_coefficient description="Maximum cruise flight lift coefficient CL_max">
+                        <value>0.5048791966</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </maximum_lift_coefficient>
+                    <top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
+                        <value>66532.93487</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_climb_mass>
+                    <top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
+                        <value>65612.81266</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_descent_mass>
+                    <top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
+                        <value>194351.2576</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>4537400</upper_boundary>
+                    </top_of_climb_range>
+                    <top_of_descent_range description="Flown range from takeoff to top of descent">
+                        <value>1272978.151</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>4537400</upper_boundary>
+                    </top_of_descent_range>
+                    <cruise_steps description="Cruise step information">
+                        <cruise_step ID="0" description="Data of a cruise step">
+                            <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </relative_end_of_cruise_step>
+                            <altitude description="Altitude of cruise step">
+                                <value>10668.00002</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>15000</upper_boundary>
+                            </altitude>
+                        </cruise_step>
+                    </cruise_steps>
+                </cruise>
+            </study_mission>
+        </mission>
+    </analysis>
+    <component_design>
+        <global_reference_point>
+            <reference_component description="Global reference point of aircraft geometry">
+                <value>fuselage</value>
+            </reference_component>
+            <x description="X coordinate of the global reference point">
+                <value>0</value>
+                <unit>m</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </x>
+            <y description="Y coordinate of the global reference point">
+                <value>0</value>
+                <unit>m</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </y>
+            <z description="Z coordinate of the global reference point">
+                <value>0</value>
+                <unit>m</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </z>
+        </global_reference_point>
+        <wing>
+            <mass_properties description="mass_properties of component wing">
+                <mass description="component mass">
+                    <value>7896.746484</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="component inertia referred to local center of gravity">
+                    <j_xx description="wing inertia in x">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="wing inertia in y">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="wing inertia in z">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="wing inertia in xy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="wing inertia in xz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="wing inertia in yx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="wing inertia in yz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="wing inertia in zx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="wing inertia in zy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                    <x description="x position of center of gravity">
+                        <value>21.92220256</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </x>
+                    <y description="y position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </y>
+                    <z description="z position of center of gravity">
+                        <value>-0.7035726591</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <position description="position of wing">
+                <x description="x position">
+                    <value>17.75145044</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </x>
+                <y description="y position">
+                    <value>0</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </y>
+                <z description="z position">
+                    <value>-1.030571436</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </z>
+            </position>
+            <specific>
+                <geometry>
+                    <aerodynamic_surface ID="0" description="main_wing">
+                        <name description="name of surface">
+                            <value>main_wing</value>
+                        </name>
+                        <position description="reference position in aircraft coordinates">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <parameters description="aerodynamic surface parameters">
+                            <direction description="unit vector according to aircraft coordinate system for direction applied at position">
+                                <x description="x direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y direction of unit vector">
+                                    <value>-1</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </direction>
+                            <symmetric description="symmetric to local x-z plane">
+                                <value>true</value>
+                            </symmetric>
+                            <sections description="sections">
+                                <section ID="0">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>6.458219551</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1.00040016</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                                <section ID="1">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-1.983993414</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>6.458219551</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1.00040016</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                                <section ID="2">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>2.035403072</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0.2355374897</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-5.352336445</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>4.599343857</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>0.9209974332</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                                <section ID="3">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>8.734380802</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>1.108838412</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-17.84112148</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>1.097897324</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>0.6265964242</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                            </sections>
+                            <spars>
+                                <spar ID="0" description="front_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                                <spar ID="1" description="rear_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                            </spars>
+                            <control_devices>
+                                <control_device ID="0" description="slat">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.1134274706</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.294</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.6981317008</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="1" description="slat">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.306</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.95</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.6981317008</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="2" description="flap_fowler">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.1134274706</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.297</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="3" description="flap_fowler">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.303</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.78</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="4" description="aileron">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.8</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.98</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>-0.3490658504</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.3490658504</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="5" description="spoiler_ground">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.2037137353</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.294</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="6" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.306</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.4195</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="7" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.4195</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.533</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="8" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.533</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.6465</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="9" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.6465</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.76</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                            </control_devices>
+                        </parameters>
+                    </aerodynamic_surface>
+                </geometry>
+            </specific>
+        </wing>
+        <empennage>
+            <position description="position of empennage">
+                <x description="x position">
+                    <value>41.19599159</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </x>
+                <y description="y position">
+                    <value>0</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </y>
+                <z description="z position">
+                    <value>0.92429206</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="mass_properties of component Conventional tail overall mass">
+                <mass description="component mass">
+                    <value>983.6646752</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="component inertia referred to local center of gravity">
+                    <j_xx description="Conventional tail overall mass inertia in x">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Conventional tail overall mass inertia in y">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Conventional tail overall mass inertia in z">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Conventional tail overall mass inertia in xy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Conventional tail overall mass inertia in xz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Conventional tail overall mass inertia in yx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Conventional tail overall mass inertia in yz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Conventional tail overall mass inertia in zx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Conventional tail overall mass inertia in zy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                    <x description="x position of center of gravity">
+                        <value>45.24364245</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </x>
+                    <y description="y position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </y>
+                    <z description="z position of center of gravity">
+                        <value>3.000638678</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific>
+                <geometry>
+                    <aerodynamic_surface ID="0" description="vertical_stabiliser">
+                        <name description="name of surface">
+                            <value>vertical_stabiliser</value>
+                        </name>
+                        <position description="reference position in aircraft coordinates">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <parameters description="aerodynamic surface parameters">
+                            <direction description="unit vector according to aircraft coordinate system for direction applied at position">
+                                <x description="x direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z direction of unit vector">
+                                    <value>-1</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </direction>
+                            <symmetric description="symmetric to local x-z plane">
+                                <value>false</value>
+                            </symmetric>
+                            <sections description="sections">
+                                <section ID="0">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>5.31423154</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                                <section ID="1">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>4.81324168</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-6.387387456</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>1.409334205</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                            </sections>
+                            <spars>
+                                <spar ID="0" description="front_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                                <spar ID="1" description="rear_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                            </spars>
+                            <control_devices>
+                                <control_device ID="0" description="rudder">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.9</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>-0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                            </control_devices>
+                        </parameters>
+                        <mass_properties description="mass_properties of component vertical stabiliser mass">
+                            <mass description="component mass">
+                                <value>417.1115867</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </mass>
+                            <inertia description="component inertia referred to local center of gravity">
+                                <j_xx description="vertical stabiliser mass inertia in x">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="vertical stabiliser mass inertia in y">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="vertical stabiliser mass inertia in z">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="vertical stabiliser mass inertia in xy">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="vertical stabiliser mass inertia in xz">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="vertical stabiliser mass inertia in yx">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="vertical stabiliser mass inertia in yz">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="vertical stabiliser mass inertia in zx">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="vertical stabiliser mass inertia in zy">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                                <x description="x position of center of gravity">
+                                    <value>44.44562535</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y position of center of gravity">
+                                    <value>0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z position of center of gravity">
+                                    <value>3.499710377</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </aerodynamic_surface>
+                    <aerodynamic_surface ID="1" description="horizontal_stabiliser">
+                        <name description="name of surface">
+                            <value>horizontal_stabiliser</value>
+                        </name>
+                        <position description="reference position in aircraft coordinates">
+                            <x description="x coordinate of point">
+                                <value>2.3164928</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>-0.5869856587</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <parameters description="aerodynamic surface parameters">
+                            <direction description="unit vector according to aircraft coordinate system for direction applied at position">
+                                <x description="x direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y direction of unit vector">
+                                    <value>-1</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </direction>
+                            <symmetric description="symmetric to local x-z plane">
+                                <value>true</value>
+                            </symmetric>
+                            <sections description="sections">
+                                <section ID="0">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>3.497738739</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                                <section ID="1">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>3.259282429</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0.3947538294</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-5.645242769</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>0.9870618726</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                            </sections>
+                            <spars>
+                                <spar ID="0" description="front_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                                <spar ID="1" description="rear_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                            </spars>
+                            <control_devices>
+                                <control_device ID="0" description="elevator">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.2</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.9</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>-0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                            </control_devices>
+                        </parameters>
+                        <mass_properties description="mass_properties of component horizontal stabiliser mass">
+                            <mass description="component mass">
+                                <value>566.5530885</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </mass>
+                            <inertia description="component inertia referred to local center of gravity">
+                                <j_xx description="horizontal stabiliser mass inertia in x">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="horizontal stabiliser mass inertia in y">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="horizontal stabiliser mass inertia in z">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="horizontal stabiliser mass inertia in xy">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="horizontal stabiliser mass inertia in xz">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="horizontal stabiliser mass inertia in yx">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="horizontal stabiliser mass inertia in yz">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="horizontal stabiliser mass inertia in zx">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="horizontal stabiliser mass inertia in zy">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                                <x description="x position of center of gravity">
+                                    <value>45.83116405</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y position of center of gravity">
+                                    <value>0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z position of center of gravity">
+                                    <value>2.633208702</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </aerodynamic_surface>
+                </geometry>
+            </specific>
+        </empennage>
+        <propulsion>
+            <position description="Reference position of the propulsion assembly">
+                <x description="x coordinate of point">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </x>
+                <y description="y coordinate of point">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </y>
+                <z description="z coordinate of point">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of the propulsion assembly">
+                <mass description="mass of the of the component">
+                    <value>9147.202805</value>
+                    <unit>kg</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of the component in respect to the CG">
+                    <j_xx description="inertia of the component">
+                        <value>357715.0023</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="inertia of the component">
+                        <value>15621.01016</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="inertia of the component">
+                        <value>364726.4249</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="inertia of the component">
+                        <value>-0.06634606414</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="inertia of the component">
+                        <value>3560.102271</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="inertia of the component">
+                        <value>-0.06634606414</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="inertia of the component">
+                        <value>-0.009678976632</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="inertia of the component">
+                        <value>3560.102271</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="inertia of the component">
+                        <value>-0.009678976632</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                    <x description="x coordinate of the center of gravity">
+                        <value>18.31595065</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </x>
+                    <y description="y coordinate of the center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </y>
+                    <z description="z coordinate of the center of gravity">
+                        <value>-2.356641711</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific>
+                <propulsion ID="0" description="Description of one propulsion">
+                    <nacelle ID="0" description="Nacelle of the propulsion assembly">
+                        <position description="Origin of the nacelle RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="Normal direction of the nacelle in the global aircraft coordinate system">
+                            <x description="x direction of unit vector">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="Geometrical description nacelle sections">
+                            <section ID="0">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.261851375</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.261851375</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0.8618070959</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.736840163</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.736840163</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="2">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>2.585421288</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.736840163</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.736840163</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="3">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>3.447228384</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.261851375</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.261851375</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the nacelle">
+                            <mass description="mass of the of the component">
+                                <value>1077.525351</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>49.05540588</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>51.64642853</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>51.6456818</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.002397325367</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0.006676311088</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.002397325367</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.002390716634</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0.006676311088</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.002390716634</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>18.03856294</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>-6.198639603</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.540481562</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </nacelle>
+                    <pylon ID="0" description="pylon of the propulsion assembly">
+                        <position description="Position of the pylon RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="unit vector according to aircraft coordinate system for direction applied at position">
+                            <x description="x direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>-1.130925687</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="sections">
+                            <section ID="0">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0.8618070959</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>1.675831273e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.368420082</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.447228384</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>3.925861338</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>2.210030553e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.804626897</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.447228384</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the pylon">
+                            <mass description="mass of the of the component">
+                                <value>529.9702159</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>0.1461895291</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>8.726965415</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>8.731134911</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.0307757067</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0.5146596874</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.0307757067</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.002448771663</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0.5146596874</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.002448771663</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>20.43239715</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>-6.198639603</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-0.9539580722</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </pylon>
+                    <engine>
+                        <model description="Name of selected engine model">
+                            <value>PW1127G-JM-H2</value>
+                        </model>
+                        <position description="Position of the engine in the global coordinate system">
+                            <x description="x coordinate of point">
+                                <value>16.31494874</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>-6.198639603</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>-2.540481562</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of the engine">
+                            <mass description="mass of the of the component">
+                                <value>2966.105836</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>1896.814168</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>3885.688187</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>3885.688187</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>18.03856294</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>-6.198639603</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.540481562</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <SLST description="Sea level static thrust of the engine">
+                            <value>123616.7566</value>
+                            <unit>N</unit>
+                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </SLST>
+                        <scale_factor description="Scale factor of the engine">
+                            <value>1.03432867</value>
+                            <unit>1</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </scale_factor>
+                        <bucket_point description="Bucket point of the engine at initial cruise flight phase">
+                            <thrust description="Thrust of the engine at the bucket point">
+                                <value>21693.35253</value>
+                                <unit>N</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </thrust>
+                            <tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
+                                <value>5.45681508e-06</value>
+                                <unit>kg/Ns</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </tsfc>
+                        </bucket_point>
+                    </engine>
+                </propulsion>
+                <propulsion ID="1" description="Description of one propulsion">
+                    <nacelle ID="0" description="Nacelle of the propulsion assembly">
+                        <position description="Origin of the nacelle RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="Normal direction of the nacelle in the global aircraft coordinate system">
+                            <x description="x direction of unit vector">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="Geometrical description nacelle sections">
+                            <section ID="0">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.261851375</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.261851375</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0.8618070959</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.736840163</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.736840163</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="2">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>2.585421288</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.736840163</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.736840163</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="3">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>3.447228384</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.261851375</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.261851375</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the nacelle">
+                            <mass description="mass of the of the component">
+                                <value>1077.525351</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>49.05540588</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>51.64642853</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>51.6456818</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.002397325367</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0.006676311088</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.002397325367</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.002390716634</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0.006676311088</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.002390716634</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>18.03856294</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>6.198639603</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.540481562</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </nacelle>
+                    <pylon ID="0" description="pylon of the propulsion assembly">
+                        <position description="Position of the pylon RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="unit vector according to aircraft coordinate system for direction applied at position">
+                            <x description="x direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>-1.130925687</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="sections">
+                            <section ID="0">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0.8618070959</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>1.675831273e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.368420082</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.447228384</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>3.925861338</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>2.210030553e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.804626897</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.447228384</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the pylon">
+                            <mass description="mass of the of the component">
+                                <value>529.9702159</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>0.1461895291</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>8.726965415</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>8.731134911</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.0307757067</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0.5146596874</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.0307757067</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.002448771663</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0.5146596874</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.002448771663</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>20.43239715</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>6.198639603</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-0.9539580722</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </pylon>
+                    <engine>
+                        <model description="Name of selected engine model">
+                            <value>PW1127G-JM-H2</value>
+                        </model>
+                        <position description="Position of the engine in the global coordinate system">
+                            <x description="x coordinate of point">
+                                <value>16.31494874</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>6.198639603</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>-2.540481562</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of the engine">
+                            <mass description="mass of the of the component">
+                                <value>2966.105836</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>1896.814168</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>3885.688187</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>3885.688187</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>18.03856294</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>6.198639603</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.540481562</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <SLST description="Sea level static thrust of the engine">
+                            <value>123616.7566</value>
+                            <unit>N</unit>
+                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </SLST>
+                        <scale_factor description="Scale factor of the engine">
+                            <value>1.03432867</value>
+                            <unit>1</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </scale_factor>
+                        <bucket_point description="Bucket point of the engine at initial cruise flight phase">
+                            <thrust description="Thrust of the engine at the bucket point">
+                                <value>21693.35253</value>
+                                <unit>N</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </thrust>
+                            <tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
+                                <value>5.45681508e-06</value>
+                                <unit>kg/Ns</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </tsfc>
+                        </bucket_point>
+                    </engine>
+                </propulsion>
+            </specific>
+        </propulsion>
+        <systems>
+            <mass_properties description="mass_properties of component systems">
+                <mass description="component mass">
+                    <value>6615.723065</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </mass>
+                <inertia description="component inertia referred to local center of gravity">
+                    <j_xx description="systems inertia in x">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="systems inertia in y">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="systems inertia in z">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="systems inertia in xy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="systems inertia in xz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="systems inertia in yx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="systems inertia in yz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="systems inertia in zx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="systems inertia in zy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                    <x description="x position of center of gravity">
+                        <value>10.49455393</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </x>
+                    <y description="y position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </y>
+                    <z description="z position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <operator_items>
+                <operator_item ID="0">
+                    <name description="name of the operator item">
+                        <value>water_and_toilet_chemicals</value>
+                    </name>
+                    <mass_properties description="mass_properties of component water and toilet chemicals">
+                        <mass description="component mass">
+                            <value>244.8</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </mass>
+                        <inertia description="component inertia referred to local center of gravity">
+                            <j_xx description="water and toilet chemicals inertia in x">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xx>
+                            <j_yy description="water and toilet chemicals inertia in y">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yy>
+                            <j_zz description="water and toilet chemicals inertia in z">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zz>
+                            <j_xy description="water and toilet chemicals inertia in xy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xy>
+                            <j_xz description="water and toilet chemicals inertia in xz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xz>
+                            <j_yx description="water and toilet chemicals inertia in yx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yx>
+                            <j_yz description="water and toilet chemicals inertia in yz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yz>
+                            <j_zx description="water and toilet chemicals inertia in zx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zx>
+                            <j_zy description="water and toilet chemicals inertia in zy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                            <x description="x position of center of gravity">
+                                <value>3.229109776</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                    </mass_properties>
+                </operator_item>
+                <operator_item ID="1">
+                    <name description="name of the operator item">
+                        <value>residual_oil_and_fuel</value>
+                    </name>
+                    <mass_properties description="mass_properties of component water and toilet chemicals">
+                        <mass description="component mass">
+                            <value>2.799540704</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </mass>
+                        <inertia description="component inertia referred to local center of gravity">
+                            <j_xx description="water and toilet chemicals inertia in x">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xx>
+                            <j_yy description="water and toilet chemicals inertia in y">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yy>
+                            <j_zz description="water and toilet chemicals inertia in z">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zz>
+                            <j_xy description="water and toilet chemicals inertia in xy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xy>
+                            <j_xz description="water and toilet chemicals inertia in xz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xz>
+                            <j_yx description="water and toilet chemicals inertia in yx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yx>
+                            <j_yz description="water and toilet chemicals inertia in yz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yz>
+                            <j_zx description="water and toilet chemicals inertia in zx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zx>
+                            <j_zy description="water and toilet chemicals inertia in zy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                            <x description="x position of center of gravity">
+                                <value>21.92220256</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                    </mass_properties>
+                </operator_item>
+            </operator_items>
+            <specific>
+                <geometry>
+                    <mass_properties>
+                        <fuel_system description="mass of ATA-28">
+                            <value>476.7269182</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </fuel_system>
+                        <de_icing description="mass of ATA-30">
+                            <value>50.0353201</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </de_icing>
+                        <lighting description="mass of ATA-33">
+                            <value>255.9890824</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </lighting>
+                        <fire_protection description="mass of ATA-26">
+                            <value>89.90290824</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </fire_protection>
+                        <oxygen_system description="mass of ATA-35">
+                            <value>114.784</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </oxygen_system>
+                        <flight_controls description="mass of ATA-27">
+                            <value>706.182169</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </flight_controls>
+                        <instruments description="mass of ATA31">
+                            <value>93.41552608</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </instruments>
+                        <automatic_flight_system description="mass of ATA22">
+                            <value>151.8002299</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </automatic_flight_system>
+                        <navigation description="mass of ATA34">
+                            <value>618.8778603</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </navigation>
+                        <communication description="mass of ATA23">
+                            <value>303.6004598</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </communication>
+                        <bleed_air_system description="mass of ATA-36">
+                            <value>219.7746979</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </bleed_air_system>
+                        <hydraulic_generation description="mass of ATA-29">
+                            <value>178.2241792</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </hydraulic_generation>
+                        <hydraulic_distribution description="mass of ATA-29">
+                            <value>715.1778549</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </hydraulic_distribution>
+                        <electrical_generation description="mass of ATA-24">
+                            <value>763.2564568</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </electrical_generation>
+                        <electrical_distribution description="mass of ATA-24">
+                            <value>645.1221143</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </electrical_distribution>
+                        <auxiliary_power_unit description="mass of ATA-49">
+                            <value>220.4595807</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </auxiliary_power_unit>
+                        <air_conditioning description="mass of ATA-21">
+                            <value>764.7941666</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </air_conditioning>
+                    </mass_properties>
+                </geometry>
+                <maximium_power_demand description="maximum power (hydraulic + electric) demand">
+                    <value>372179.1673</value>
+                    <unit>W</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </maximium_power_demand>
+                <maximium_bleed_air_demand description="maximum bleed air demand">
+                    <value>2.397104381</value>
+                    <unit>kg/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </maximium_bleed_air_demand>
+                <average_power_demand description="average power (hydraulic + electric) demand">
+                    <value>125700.3236</value>
+                    <unit>W</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </average_power_demand>
+                <average_bleed_air_demand description="average bleed air demand">
+                    <value>1.024591634</value>
+                    <unit>kg/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </average_bleed_air_demand>
+            </specific>
+        </systems>
+        <fuselage description="Geometric description of the aircraft fuselage." tool_level="1">
+            <position description="Position of the fuselages with regard to the global reference point.">
+                <x description="Distance in x direction with regard to the global reference point. (fuselage nose point)">
+                    <value>-0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-100</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </x>
+                <y description="Distance in y direction with regard to the global reference point. (fuselage nose point)">
+                    <value>-0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-25</lower_boundary>
+                    <upper_boundary>25</upper_boundary>
+                </y>
+                <z description="Distance in z direction with regard to the global reference point. (fuselage nose point)">
+                    <value>-0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-5</lower_boundary>
+                    <upper_boundary>5</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of all fuselages.">
+                <mass description="Mass of all fuselages.">
+                    <value>22532.25982</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of all fuselages with regard to the total center of gravity.">
+                    <j_xx description="Inertia of the of all fuselages in x.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Inertia of the of all fuselages in y.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Inertia of the of all fuselages in z.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Inertia of all fuselages in xy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Inertia of all fuselages in xz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Inertia of all fuselages in yx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Inertia of all fuselages in yz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Inertia of all fuselages in zx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Inertia of all fuselages in zy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of all fuselages.">
+                    <x description="Center of gravity in x-direction with regard to the global reference point. (of all fuselages)">
+                        <value>21.6379044</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>50</upper_boundary>
+                    </x>
+                    <y description="Center of gravity in y-direction with regard to the global reference point. (of all fuselages)">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-5</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </y>
+                    <z description="Center of gravity in z-direction with regard to the global reference point. (of all fuselages)">
+                        <value>-0.2413</value>
+                        <unit>m</unit>
+                        <lower_boundary>-5</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific description="Fuselage design specific output parameter.">
+                <geometry description="Geometry description of the entire fuselage design.">
+                    <fuselage ID="0" description="Geometrical description of one entire fuselage.">
+                        <name description="Name of the fuselage.">
+                            <value>fuselage_0</value>
+                        </name>
+                        <position description="Position of one entire fuselage with regard to the fuselage global position.">
+                            <x description="Distance in x direction with regard to the fuselage gear global position.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the fuselage gear global position.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-25</lower_boundary>
+                                <upper_boundary>25</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the fuselage gear global position.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </position>
+                        <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                            <x description="X component of the unit vector.">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </x>
+                            <y description="Y component of the unit vector.">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </y>
+                            <z description="Z component of the unit vector.">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </z>
+                        </direction>
+                        <mass_properties description="Mass properties of one entire fuselage.">
+                            <mass description="Mass of one entire fuselage.">
+                                <value>22532.259823558</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>100000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire fuselage with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire fuselage in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire fuselage in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire fuselage in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire fuselage in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire fuselage in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire fuselage in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire fuselage in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire fuselage in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire fuselage in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire fuselage.">
+                                <x description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-25</lower_boundary>
+                                    <upper_boundary>25</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <sections description="Geometrical description of the fuselage sections of one entire fuselage.">
+                            <section ID="0" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_0</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.957580772</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.068075648</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.236859405</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.267845269</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>0.496500597</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="1" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_1</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.924669034</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.192850112</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.410780143</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.467251904</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>0.836740921</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="2" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_2</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.88671607</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.325974005</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.51432337</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.617142191</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.09949371</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="3" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_3</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.814819481</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.552671561</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.638938798</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.811819183</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.332869486</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="4" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_4</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.746964181</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.779068819</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.756396515</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.976541153</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.597847703</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="5" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_5</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.624593025</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>1.123655542</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.945319536</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.211739628</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.950706682</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="6" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_6</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.499674101</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>1.438280013</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.097107435</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.430154001</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>2.243644807</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="7" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_7</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.21769763</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>2.128158942</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.34967515</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.867790838</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>2.796234326</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="8" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_8</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.174885536</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>2.619107088</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.558414858</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.972433715</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.095828445</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="9" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_9</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.083279283</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>3.445878719</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.734079899</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.114075921</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.508608277</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="10" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_10</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.041639641</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>4.194982413</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.833938046</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.167619711</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.762303773</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="11" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_11</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>5.168818078</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.877197398</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.219703367</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.908262138</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="12" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_12</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>6.2175644</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915417119</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227583628</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="13" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_13</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>6.2175644</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915417119</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227583628</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="14" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_14</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>38.14663462</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915413925</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227579912</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="15" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_15</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>38.14663462</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915413925</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227579912</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="16" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_16</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>42.57228328</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.699062858</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.736999316</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.3288491</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="17" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_17</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>43.42065009</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.657090968</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.517589228</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.095828445</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="18" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_18</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>45.11738369</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.575335554</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.93980933</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>2.46334671</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="19" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_19</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0.92429206</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>48.07829878</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.528165979</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.614244216</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>0.559150813</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                        </sections>
+                        <number_of_required_cabin_crew description="Number of minimum required flight attendants.">
+                            <value>4</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </number_of_required_cabin_crew>
+                        <number_of_required_flight_crew description="Number of minimum required flight crew members.">
+                            <value>2</value>
+                            <unit>1</unit>
+                            <lower_boundary>1</lower_boundary>
+                            <upper_boundary>4</upper_boundary>
+                        </number_of_required_flight_crew>
+                        <mass_breakdown description="Mass breakdown of fuselage design module in accordance to CPACS.">
+                            <fuselage_structure description="Mass breakdown of the fuselage structure block.">
+                                <component_mass ID="0" description="Mass of a single component of the fuselage structure block.">
+                                    <name description="Name of the fuselage structure component.">
+                                        <value>door_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage structure component.">
+                                        <value>360.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="1" description="Mass of a single component of the fuselage structure block.">
+                                    <name description="Name of the fuselage structure component.">
+                                        <value>fuselage_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage structure component.">
+                                        <value>14716.991711297</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                            </fuselage_structure>
+                            <fuselage_furnishing description="Mass breakdown of the fuselage furnishing block.">
+                                <component_mass ID="0" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>lavatory_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>290.01</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="1" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>flight_attendant_seat_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>48.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="2" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>floor_covering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>159.641751426</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="3" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>wall_covering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>289.30950138</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="4" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>ceiling_covering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>106.98516576</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="5" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>linings_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>396.29466714</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="6" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>acoustic_and_thermal_insolation_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>619.575445338</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="7" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>overhead_bin_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>351.213928</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="8" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>passenger_safety_unit_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>90.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="9" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>lightning_panel_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>72.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="10" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>oxygen_system_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>201.51999999999998</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="11" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>cargo_linings_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>431.346961788</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="12" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>cargo_loadings_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>672.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="13" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>miscellaneous_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>324.160275369</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                            </fuselage_furnishing>
+                            <fuselage_operator_items description="Mass breakdown of the fuselage  operator items block.">
+                                <component_mass ID="0" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>total_emergency_equipment_masses</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>840.4850832</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="1" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>flight_attendant_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>280.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="2" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>flight_crew_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>170.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="3" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>in_flight_entertainment</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>90.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="4" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>total_fixed_galley_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>315.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="5" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>total_seat_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>1242.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="6" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>catering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>952.02</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                            </fuselage_operator_items>
+                        </mass_breakdown>
+                        <fuselage_accommodation description="Description of the accommodation of current fuselage.">
+                            <position description="Position of the payload tubes with regard to the fuselage position.">
+                                <x description="Distance in x direction with regard to the fuselage position.">
+                                    <value>3.75</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Distance in y direction with regard to the fuselage position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-0</lower_boundary>
+                                    <upper_boundary>0</upper_boundary>
+                                </y>
+                                <z description="Distance in z direction with regard to the fuselage position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <mass_properties description="Mass properties of the payload tubes of one entire fuselage.">
+                                <mass description="Mass of the payload tubes of one entire fuselage.">
+                                    <value>7455.268112261</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                                <center_of_gravity description="Center of gravity of all payload tubes.">
+                                    <x description="Center of gravity in x-direction with regard to the center of gravity of the fuselage.">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>50</upper_boundary>
+                                    </x>
+                                    <y description="Center of gravity in y-direction with regard to the center of gravity of the fuselage.">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-5</lower_boundary>
+                                        <upper_boundary>5</upper_boundary>
+                                    </y>
+                                    <z description="Center of gravity in z-direction with regard to the center of gravity of the fuselage.">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-5</lower_boundary>
+                                        <upper_boundary>5</upper_boundary>
+                                    </z>
+                                </center_of_gravity>
+                            </mass_properties>
+                            <payload_tube ID="0" description="Geometrical description of one payload tube of the fuselage.">
+                                <name description="Name of the payload tube.">
+                                    <value>center_payload_tube</value>
+                                </name>
+                                <payload_tube_reference_points description="Payload tube center reference points in x, y and z-direction referred to fuselage nose point.">
+                                    <front_reference_points description="Reference points in the front of payload tube.">
+                                        <x description="Payload tube reference point in x-direction.">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <y description="Payload tube reference point in y-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </y>
+                                        <z description="Payload tube reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                        <upper_z description="Upper payload tube reference point in z-direction.">
+                                            <value>1.778</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </upper_z>
+                                        <lower_z description="Lower payload tube reference point in z-direction.">
+                                            <value>-2.090166</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>0</upper_boundary>
+                                        </lower_z>
+                                    </front_reference_points>
+                                    <aft_reference_points description="Reference points in the aft of payload tube.">
+                                        <x description="Payload tube reference point in x-direction.">
+                                            <value>27.016456</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <y description="Payload tube reference point in y-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </y>
+                                        <z description="Payload tube reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                        <upper_z description="Upper payload tube reference point in z-direction.">
+                                            <value>1.778</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </upper_z>
+                                        <lower_z description="Lower payload tube reference point in z-direction.">
+                                            <value>-2.090166</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>0</upper_boundary>
+                                        </lower_z>
+                                    </aft_reference_points>
+                                </payload_tube_reference_points>
+                                <payload_tube_wall_reference_points description="Payload tube wall reference points in x, y and z-direction referred to fuselage nose point.">
+                                    <front_reference_points description="Reference points in the front of payload tube.">
+                                        <x description="Wall reference point in x-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <left_y description="Left wall reference point in y-direction.">
+                                            <value>-1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </left_y>
+                                        <right_y description="Right wall reference point in y-direction.">
+                                            <value>1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </right_y>
+                                        <z description="Wall reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                    </front_reference_points>
+                                    <aft_reference_points description="Reference points in the aft of payload tube.">
+                                        <x description="Wall reference point in x-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <left_y description="Left wall reference point in y-direction.">
+                                            <value>-1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </left_y>
+                                        <right_y description="Right wall reference point in y-direction.">
+                                            <value>1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </right_y>
+                                        <z description="Wall reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                    </aft_reference_points>
+                                </payload_tube_wall_reference_points>
+                                <payload_tube_structural_wall_thickness description="Structural wall thickness of the payload tube.">
+                                    <value>0.137414</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </payload_tube_structural_wall_thickness>
+                                <payload_tube_water_volume description="Total water volume of one entire payload tube.">
+                                    <value>258.176893829</value>
+                                    <unit>m^3</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1000</upper_boundary>
+                                </payload_tube_water_volume>
+                                <payload_decks description="Geometrical description of the payload decks.">
+                                    <payload_deck ID="0" description="Geometrical description of the payload decks in one payload tube.">
+                                        <name description="Name of the payload deck.">
+                                            <value>passenger_deck_1</value>
+                                        </name>
+                                        <position description="Position of the payload deck with regard to the payload tube reference point.">
+                                            <x description="Distance in x direction with regard to the payload tube reference point.">
+                                                <value>0.0</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-100</lower_boundary>
+                                                <upper_boundary>100</upper_boundary>
+                                            </x>
+                                            <y description="Distance in y direction with regard to the payload tube reference point.">
+                                                <value>0.0</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-0</lower_boundary>
+                                                <upper_boundary>0</upper_boundary>
+                                            </y>
+                                            <z description="Distance in z direction with regard to the payload tube reference point.">
+                                                <value>-0.4826</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-5</lower_boundary>
+                                                <upper_boundary>5</upper_boundary>
+                                            </z>
+                                        </position>
+                                        <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
+                                            <value>0.206248</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1</upper_boundary>
+                                        </payload_deck_structural_floor_thickness>
+                                        <payload_deck_water_volume description="Total water volume of the payload deck.">
+                                            <value>172.1179292</value>
+                                            <unit>m^3</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1000</upper_boundary>
+                                        </payload_deck_water_volume>
+                                        <payload_deck_length description="Total length of the payload deck.">
+                                            <value>27.016456</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </payload_deck_length>
+                                        <payload_deck_required_galley_power description="Required galley power of the payload deck.">
+                                            <value>9000</value>
+                                            <unit>W</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100000</upper_boundary>
+                                        </payload_deck_required_galley_power>
+                                    </payload_deck>
+                                    <payload_deck ID="1" description="Geometrical description of the payload decks in one payload tube.">
+                                        <name description="Name of the payload deck.">
+                                            <value>cargo_deck</value>
+                                        </name>
+                                        <position description="Position of the payload deck with regard to the payload tube reference point.">
+                                            <x description="Distance in x direction with regard to the payload tube reference point.">
+                                                <value>3.75</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-100</lower_boundary>
+                                                <upper_boundary>100</upper_boundary>
+                                            </x>
+                                            <y description="Distance in y direction with regard to the payload tube reference point.">
+                                                <value>0.0</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-0</lower_boundary>
+                                                <upper_boundary>0</upper_boundary>
+                                            </y>
+                                            <z description="Distance in z direction with regard to the payload tube reference point.">
+                                                <value>-1.831848</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-5</lower_boundary>
+                                                <upper_boundary>5</upper_boundary>
+                                            </z>
+                                        </position>
+                                        <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
+                                            <value>0.206248</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1</upper_boundary>
+                                        </payload_deck_structural_floor_thickness>
+                                        <payload_deck_water_volume description="Total water volume of the payload deck.">
+                                            <value>86.05896460966666</value>
+                                            <unit>m^3</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1000</upper_boundary>
+                                        </payload_deck_water_volume>
+                                        <payload_deck_length description="Total length of the payload deck.">
+                                            <value>13.508228</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </payload_deck_length>
+                                        <payload_deck_required_galley_power description="Required galley power of the payload deck.">
+                                            <value>0</value>
+                                            <unit>W</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100000</upper_boundary>
+                                        </payload_deck_required_galley_power>
+                                    </payload_deck>
+                                </payload_decks>
+                            </payload_tube>
+                        </fuselage_accommodation>
+                    </fuselage>
+                </geometry>
+            </specific>
+        </fuselage>
+        <tank description="Description of aircraft tanks." tool_level="2">
+            <position description="Tank reference point, position of the tanks with regard to the global reference point.">
+                <x description="Distance between the foremost tank end and the global reference point in x-direction.">
+                    <value>30.584919097564068</value>
+                    <unit>m</unit>
+                    <lower_boundary>-80</lower_boundary>
+                    <upper_boundary>80</upper_boundary>
+                </x>
+                <y description="Distance between the foremost tank end and the global reference point in y-direction.">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-80</lower_boundary>
+                    <upper_boundary>80</upper_boundary>
+                </y>
+                <z description="Distance between the foremost middle tank end and the global reference point in z-direction.">
+                    <value>-0.15608300249376805</value>
+                    <unit>m</unit>
+                    <lower_boundary>-80</lower_boundary>
+                    <upper_boundary>80</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of all tanks.">
+                <mass description="Total tank mass.">
+                    <value>2099.2609847846707</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of all tanks with regard to the total center of gravity.">
+                    <j_xx description="Inertia of all tanks in x.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Inertia of all tanks in y.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Inertia of all tanks in z.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Inertia of all tanks in xy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Inertia of all tanks in xz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Inertia of all tanks in yx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Inertia of all tanks in yz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Inertia of all tanks in zx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Inertia of all tanks in zy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of all tanks.">
+                    <x description="Center of gravity in x-direction with regard to the global reference point.">
+                        <value>36.14497459013074</value>
+                        <unit>m</unit>
+                        <lower_boundary>-80</lower_boundary>
+                        <upper_boundary>80</upper_boundary>
+                    </x>
+                    <y description="Center of gravity in y-direction with regard to the global reference point.">
+                        <value>0.0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-40</lower_boundary>
+                        <upper_boundary>40</upper_boundary>
+                    </y>
+                    <z description="Center of gravity in z-direction with regard to the global reference point.">
+                        <value>-0.09421024896405661</value>
+                        <unit>m</unit>
+                        <lower_boundary>-5</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific description="Tank design specific output parameter.">
+                <additional_fuselage_length description="Additional fuselage length (if smaller than 0: shrink fuselage, if greater than 0: stretch fuselage).">
+                    <value>10.749603460904984</value>
+                    <unit>m</unit>
+                    <lower_boundary>-80</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </additional_fuselage_length>
+                <tank ID="0" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_0</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>fuselage_tail_cone</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>7.555080902</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.027267186</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>721.0907415044228</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the local reference point.">
+                                <value>1.6028937744784333</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the local reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the local reference point.">
+                                <value>0.15285862860398236</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>1.602893774</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.152858629</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>1.621076599e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>true</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>front_end_cap</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>-0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>circular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.8781485752888233</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>front_tank_section</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>-0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.878148575</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>circular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>3.4359306216476657</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>3.4359306216476657</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="2" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>rear_tank_section</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>-0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.045861048</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>2.358148575</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>circular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>3.2200412567453918</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>3.2200412567453918</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="3" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>rear_end_cap</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>-0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.045861048</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>3.194522558</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>circular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>-0.8363739831802333</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                    <mass_breakdown description="Mass breakdown of one tank.">
+                        <tank_insulation description="Mass breakdown of the tank insulation.">
+                            <component_mass ID="0" description="Mass of a single component of the tank insulation.">
+                                <name description="Name of the tank insulation component.">
+                                    <value>insulation</value>
+                                </name>
+                                <mass description="Mass of the tank insulation component.">
+                                    <value>301.2756208825662</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                            <component_mass ID="1" description="Mass of a single component of the tank insulation.">
+                                <name description="Name of the tank insulation component.">
+                                    <value>vapor_barrier</value>
+                                </name>
+                                <mass description="Mass of the tank insulation component.">
+                                    <value>24.0</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                        </tank_insulation>
+                        <tank_structure description="Mass breakdown of the tank structure.">
+                            <component_mass ID="0" description="Mass of a single component of the tank structure.">
+                                <name description="Name of the tank structure component.">
+                                    <value>wall</value>
+                                </name>
+                                <mass description="Mass of the tank structure component.">
+                                    <value>341.55512062185664</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                            <component_mass ID="1" description="Mass of a single component of the tank structure.">
+                                <name description="Name of the tank structure component.">
+                                    <value>pumps</value>
+                                </name>
+                                <mass description="Mass of the tank structure component.">
+                                    <value>9.26</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                            <component_mass ID="2" description="Mass of a single component of the tank structure.">
+                                <name description="Name of the tank structure component.">
+                                    <value>baffle</value>
+                                </name>
+                                <mass description="Mass of the tank structure component.">
+                                    <value>45.0</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                        </tank_structure>
+                    </mass_breakdown>
+                </tank>
+                <tank ID="1" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_1</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>fuselage_rear</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>1378.170243280248</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the local reference point.">
+                                <value>3.677540451217963</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the local reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the local reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>3.677540451</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>5.160300836e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>true</value>
+                    </energy_capacity_required_for_mission>
+                    <mass_breakdown description="Mass breakdown of one tank.">
+                        <tank_structure description="Mass breakdown of the tank structure.">
+                            <component_mass ID="0" description="Mass of a single component of the tank structure.">
+                                <name description="Name of the tank structure component.">
+                                    <value>wall</value>
+                                </name>
+                                <mass description="Mass of the tank structure component.">
+                                    <value>769.6176545771676</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                            <component_mass ID="1" description="Mass of a single component of the tank structure.">
+                                <name description="Name of the tank structure component.">
+                                    <value>pumps</value>
+                                </name>
+                                <mass description="Mass of the tank structure component.">
+                                    <value>9.26</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                            <component_mass ID="2" description="Mass of a single component of the tank structure.">
+                                <name description="Name of the tank structure component.">
+                                    <value>baffle</value>
+                                </name>
+                                <mass description="Mass of the tank structure component.">
+                                    <value>45.0</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                        </tank_structure>
+                        <tank_insulation description="Mass breakdown of the tank insulation.">
+                            <component_mass ID="0" description="Mass of a single component of the tank insulation.">
+                                <name description="Name of the tank insulation component.">
+                                    <value>insulation</value>
+                                </name>
+                                <mass description="Mass of the tank insulation component.">
+                                    <value>530.2925887030806</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                            <component_mass ID="1" description="Mass of a single component of the tank insulation.">
+                                <name description="Name of the tank insulation component.">
+                                    <value>vapor_barrier</value>
+                                </name>
+                                <mass description="Mass of the tank insulation component.">
+                                    <value>24.0</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                            </component_mass>
+                        </tank_insulation>
+                    </mass_breakdown>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>front_end_cap</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>-0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>circular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.902540451218</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>front_tank_section</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>-0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.902540451</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>circular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>3.5619868279999998</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>3.5619868279999998</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="2" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>rear_tank_section</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>-0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>6.452540451</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>circular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>3.5619868279999998</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>3.5619868279999998</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="3" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>rear_end_cap</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>-0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>7.355080902</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>circular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>-0.902540451218</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+            </specific>
+        </tank>
+        <landing_gear description="Geometric description of the aircraft undercarriage." tool_level="3">
+            <position description="Position of the total undercarriage arrangement with regard to the global reference point.">
+                <x description="Distance in x direction with regard to the global reference point. (total undercarriage arrangement)">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-100</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </x>
+                <y description="Distance in y direction with regard to the global reference point. (total undercarriage arrangement)">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-25</lower_boundary>
+                    <upper_boundary>25</upper_boundary>
+                </y>
+                <z description="Distance in z direction with regard to the global reference point. (total undercarriage arrangement)">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-10</lower_boundary>
+                    <upper_boundary>10</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of the total undercarriage arrangement.">
+                <mass description="Mass of the total undercarriage arrangement.">
+                    <value>2933.4069</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of the total undercarriage arrangement with regard to the total center of gravity.">
+                    <j_xx description="Inertia of the total undercarriage arrangement in x.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Inertia of the total undercarriage arrangement in y.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Inertia of the total undercarriage arrangement in z.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Inertia of the total undercarriage arrangement in xy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Inertia of the total undercarriage arrangement in xz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Inertia of the total undercarriage arrangement in yx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Inertia of the total undercarriage arrangement in yz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Inertia of the total undercarriage arrangement in zx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Inertia of the total undercarriage arrangement in zy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of the total undercarriage arrangement.">
+                    <x description="Center of gravity in x-direction with regard to the global reference point. (total undercarriage arrangement)">
+                        <value>20.1679</value>
+                        <unit>m</unit>
+                        <lower_boundary>-100</lower_boundary>
+                        <upper_boundary>100</upper_boundary>
+                    </x>
+                    <y description="Center of gravity in y-direction with regard to the global reference point. (total undercarriage arrangement)">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-50</lower_boundary>
+                        <upper_boundary>50</upper_boundary>
+                    </y>
+                    <z description="Center of gravity in z-direction with regard to the global reference point. (total undercarriage arrangement)">
+                        <value>-1.6454</value>
+                        <unit>m</unit>
+                        <lower_boundary>-10</lower_boundary>
+                        <upper_boundary>10</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <aircraft_classification_number description="Aircraft classification number for the total undercarriage arrangement. (CBR = [3, 6, 10, 15])">
+                <value>[53.5, 47.6, 43.5, 41.6]</value>
+            </aircraft_classification_number>
+            <specific description="Landing gear specific output parameter.">
+                <geometry description="Geometry description of the entire landing gear.">
+                    <landing_gear_assembly ID="0" description="Geometrical description of one entire landing gear leg.">
+                        <name description="Name of the landing gear leg.">
+                            <value>nose_gear_assembly</value>
+                        </name>
+                        <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+                            <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>5.2</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-50</lower_boundary>
+                                <upper_boundary>50</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-1.6572</value>
+                                <unit>m</unit>
+                                <lower_boundary>-10</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of one entire landing gear leg.">
+                            <mass description="Mass of one entire landing gear leg.">
+                                <value>441.3324</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire landing gear leg in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire landing gear leg in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire landing gear leg in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire landing gear leg in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire landing gear leg in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire landing gear leg in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire landing gear leg in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire landing gear leg in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire landing gear leg in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+                                <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>-16.0097</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-50</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.0118</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-10</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+                            <strut_diameter description="Diameter of the landing gear strut">
+                                <value>0.2248</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.0</upper_boundary>
+                            </strut_diameter>
+                            <strut_length description="Length of the landing gear strut">
+                                <value>2.0835</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </strut_length>
+                            <tire_description ID="0" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS01203</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>-0.3372</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.0835</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>0.7699</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.2248</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                            <tire_description ID="1" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS01203</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>0.3372</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.0835</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>0.7699</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.2248</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                        </assembly_components>
+                    </landing_gear_assembly>
+                    <landing_gear_assembly ID="1" description="Geometrical description of one entire landing gear leg.">
+                        <name description="Name of the landing gear leg.">
+                            <value>right_main_gear_outer_strut</value>
+                        </name>
+                        <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+                            <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>23.0031</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>4.4813</value>
+                                <unit>m</unit>
+                                <lower_boundary>-50</lower_boundary>
+                                <upper_boundary>50</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-0.8565</value>
+                                <unit>m</unit>
+                                <lower_boundary>-10</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of one entire landing gear leg.">
+                            <mass description="Mass of one entire landing gear leg.">
+                                <value>1246.0373</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire landing gear leg in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire landing gear leg in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire landing gear leg in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire landing gear leg in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire landing gear leg in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire landing gear leg in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire landing gear leg in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire landing gear leg in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire landing gear leg in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+                                <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>1.3931</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+                                    <value>4.4813</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-50</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.2162</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-10</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+                            <strut_diameter description="Diameter of the landing gear strut">
+                                <value>0.2322</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.0</upper_boundary>
+                            </strut_diameter>
+                            <strut_length description="Length of the landing gear strut">
+                                <value>2.8842</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </strut_length>
+                            <tire_description ID="0" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>-0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.8842</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                            <tire_description ID="1" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.8842</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                        </assembly_components>
+                    </landing_gear_assembly>
+                    <landing_gear_assembly ID="2" description="Geometrical description of one entire landing gear leg.">
+                        <name description="Name of the landing gear leg.">
+                            <value>left_main_gear_outer_strut</value>
+                        </name>
+                        <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+                            <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>23.0031</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-4.4813</value>
+                                <unit>m</unit>
+                                <lower_boundary>-50</lower_boundary>
+                                <upper_boundary>50</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-0.8565</value>
+                                <unit>m</unit>
+                                <lower_boundary>-10</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of one entire landing gear leg.">
+                            <mass description="Mass of one entire landing gear leg.">
+                                <value>1246.0373</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire landing gear leg in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire landing gear leg in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire landing gear leg in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire landing gear leg in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire landing gear leg in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire landing gear leg in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire landing gear leg in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire landing gear leg in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire landing gear leg in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+                                <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>1.3931</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+                                    <value>4.4813</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-50</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.2162</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-10</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+                            <strut_diameter description="Diameter of the landing gear strut">
+                                <value>0.2322</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.0</upper_boundary>
+                            </strut_diameter>
+                            <strut_length description="Length of the landing gear strut">
+                                <value>2.8842</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </strut_length>
+                            <tire_description ID="0" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>-0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.8842</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                            <tire_description ID="1" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.8842</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                        </assembly_components>
+                    </landing_gear_assembly>
+                </geometry>
+            </specific>
+        </landing_gear>
+    </component_design>
+    <sizing_point>
+        <thrust_to_weight description="Total thrust (kN) divided by maximum aircraft weight (kN)">
+            <value>0.3364390052</value>
+            <unit>1</unit>
+            <lower_boundary>-1.797693135e+308</lower_boundary>
+            <upper_boundary>1.797693135e+308</upper_boundary>
+        </thrust_to_weight>
+        <wing_loading description="Maximum takeoff mass (MTOM) divided by wing area (Sref)">
+            <value>560</value>
+            <unit>kg/m^2</unit>
+            <lower_boundary>-inf</lower_boundary>
+            <upper_boundary>inf</upper_boundary>
+        </wing_loading>
+    </sizing_point>
+    <assessment description="Assessment data">
+        <performance description="Assessment of performance values">
+            <takeoff description="Takeoff assessment">
+                <takeoff_distance_normal_safety description="Takeoff distance at Sea Level for MTOM and (ISA + deltaISA)-Conditions(calculated by mission_analysis using missionDesign.xml settings) with all engines operating (AEO)">
+                    <value>907.8759565</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </takeoff_distance_normal_safety>
+                <lift_off_speed_velocity description="Lift off velocity">
+                    <value>65.20930452</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>400</upper_boundary>
+                </lift_off_speed_velocity>
+                <takeoff_safety_speed description="Take off safety speed (V2)">
+                    <value>65.20930452</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>200</upper_boundary>
+                </takeoff_safety_speed>
+                <final_takeoff_speed description="Final take off speed">
+                    <value>95.38595077</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>200</upper_boundary>
+                </final_takeoff_speed>
+                <time_to_screen_height description="Time to screen height">
+                    <value>28.52834443</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>3600</upper_boundary>
+                </time_to_screen_height>
+                <climb_or_descend_segment_climb_gradient description="Climb or descend in second segment">
+                    <value>3.93217426</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </climb_or_descend_segment_climb_gradient>
+                <final_segment_climb_gradient description="Climb gradient in final segment">
+                    <value>3.93217426</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </final_segment_climb_gradient>
+            </takeoff>
+            <altitude description="Assessment of altitude related values">
+                <maximum_operating_altitude description="Maximum operating altitude (100 ft/min rate of climb)">
+                    <value>12545.57013</value>
+                    <unit>m</unit>
+                    <lower_boundary>4500</lower_boundary>
+                    <upper_boundary>20000</upper_boundary>
+                </maximum_operating_altitude>
+                <maximum_ceiling_altitude description="Maximum operating altitude (50 ft/min rate of climb)">
+                    <value>12660.55488</value>
+                    <unit>m</unit>
+                    <lower_boundary>4500</lower_boundary>
+                    <upper_boundary>20000</upper_boundary>
+                </maximum_ceiling_altitude>
+                <maximum_altitude_one_engine_inoperative description="Maximum operating altitude with one engine inoperative (100 ft/min rate of climb)">
+                    <value>6415.414758</value>
+                    <unit>m</unit>
+                    <lower_boundary>1500</lower_boundary>
+                    <upper_boundary>12000</upper_boundary>
+                </maximum_altitude_one_engine_inoperative>
+            </altitude>
+            <climb description="Assessment of the climb segment">
+                <design_time_to_climb description="Time needed to climb from 1500ft to ICA (ISA + deltaISA)">
+                    <value>1050.354193</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>7200</upper_boundary>
+                </design_time_to_climb>
+                <time_to_1500ft_ISA description="Time needed to climb from break release to 1500ft (ISA + deltaISA)">
+                    <value>69.18025702</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>7200</upper_boundary>
+                </time_to_1500ft_ISA>
+                <time_to_ICA_ISA description="Time needed to climb from break release to ICA (ISA + deltaISA)">
+                    <value>1119.53445</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>7200</upper_boundary>
+                </time_to_ICA_ISA>
+                <range_to_ICA_ISA description="Range needed to climb from break release to ICA (ISA + deltaISA)">
+                    <value>208170.2184</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>500000</upper_boundary>
+                </range_to_ICA_ISA>
+                <fuel_to_ICA_ISA description="Fuel mass needed to climb from break release to ICA (ISA + deltaISA)">
+                    <value>502.5839811</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>10000</upper_boundary>
+                </fuel_to_ICA_ISA>
+            </climb>
+            <speed>
+                <maximum_operating_mach_number description="Maximum operating mach number">
+                    <value>0.82</value>
+                    <unit>1</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1</upper_boundary>
+                </maximum_operating_mach_number>
+                <maximum_operating_velocity description="Maximum operating velocity">
+                    <value>180</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>400</upper_boundary>
+                </maximum_operating_velocity>
+                <dive_mach_number description="Maximum dive mach number">
+                    <value>0.902</value>
+                    <unit>1</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1</upper_boundary>
+                </dive_mach_number>
+                <dive_velocity description="Dive velocity">
+                    <value>198</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>400</upper_boundary>
+                </dive_velocity>
+                <one_g_stall_speed_velocity description="One g stall speed">
+                    <value>74.39186581</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>400</upper_boundary>
+                </one_g_stall_speed_velocity>
+            </speed>
+            <landing>
+                <needed_runway_length description="Needed runway length">
+                    <value>1495.151103</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>100000</upper_boundary>
+                </needed_runway_length>
+                <approach_speed description="Approach speed">
+                    <value>60.48885847</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1000</upper_boundary>
+                </approach_speed>
+            </landing>
+            <range>
+                <range_max_payload_at_maximum_takeoff_mass description="Range at max payload at maximum take off mass">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </range_max_payload_at_maximum_takeoff_mass>
+                <range_max_fuel_at_maximum_takeoff_mass description="Range at max fuel at maximum take off mass">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </range_max_fuel_at_maximum_takeoff_mass>
+                <payload_maximum_fuel_at_maximum_takeoff_mass description="Payload at maximum fuel at maximum takeoff mass">
+                    <value>0</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </payload_maximum_fuel_at_maximum_takeoff_mass>
+                <range_maximum_fuel_empty description="Range at maximum fuel empty">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </range_maximum_fuel_empty>
+            </range>
+        </performance>
+        <ecological_assessment description="Ecological assessment data" />
+        <operating_cost_estimation_tu_berlin description="Operating costs (sum of direct and indirect operating costs)" tool_level="2">
+            <direct_operating_costs description="Direct operating costs (sum of route independent and route dependent costs)">
+                <direct_operating_costs_annual description="Direct operating costs (DOC) per year">
+                    <value>30</value>
+                    <unit>EUR/y</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </direct_operating_costs_annual>
+            </direct_operating_costs>
+            <indirect_operating_costs description="Indirect operating costs (IOC)">
+                <indirect_operating_costs_annual description="Indirect operating costs (IOC) per year">
+                    <value>40</value>
+                    <unit>EUR/y</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </indirect_operating_costs_annual>
+            </indirect_operating_costs>
+        </operating_cost_estimation_tu_berlin>
+    </assessment>
+    <requirement_compliance description="Compliance of given requirements">
+        <top_level_aircraft_requirements description="Compliance of top level aircraft requirements">
+            <initial_cruise_altitude description="Compliance check of the initial cruise altitude.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </initial_cruise_altitude>
+            <initial_cruise_mach_number description="Compliance check of the initial cruise mach number.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </initial_cruise_mach_number>
+            <maximum_operating_altitude description="Compliance check of the maximum operating altitude.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </maximum_operating_altitude>
+            <maximum_altitude_one_engine_inoperative description="Compliance check of the maximum altitude one engine inoperative.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </maximum_altitude_one_engine_inoperative>
+            <design_time_to_climb description="Compliance check of the design time to climb.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </design_time_to_climb>
+            <design_takeoff_distance description="Compliance check of the design takeoff distance.">
+                <maintainable description="Switch indicating if design takeoff distance can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </design_takeoff_distance>
+            <design_landing_field_length description="Compliance check of the design landing field length.">
+                <maintainable description="Switch indicating if landing field length can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </design_landing_field_length>
+            <design_approach_speed description="Compliance check of the design approach speed.">
+                <maintainable description="Switch indicating if approach speed can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </design_approach_speed>
+            <span_limit>
+                <maintainable description="Switch indicating if the span limit according to ICAO aerodrome ref code is maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </span_limit>
+        </top_level_aircraft_requirements>
+        <certification>
+            <climb_gradient_of_second_takeoff_segment>
+                <maintainable description="Switch indicating if climb gradient of second takeoff segment can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </climb_gradient_of_second_takeoff_segment>
+            <climb_gradient_of_final_takeoff_segment>
+                <maintainable description="Switch indicating if climb gradient of final takeoff segment can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </climb_gradient_of_final_takeoff_segment>
+            <climb_gradient_approach_one_engine_inoperative>
+                <maintainable description="Switch indicating if climb gradient approach one engine inoperative can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </climb_gradient_approach_one_engine_inoperative>
+            <climb_gradient_all_engines_operative>
+                <maintainable description="Switch indicating if climb gradient with all engines operative can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </climb_gradient_all_engines_operative>
+        </certification>
+    </requirement_compliance>
+</aircraft_exchange_file>
\ No newline at end of file
diff --git a/docs/get-involved/modularization/python-template/projects/UNICADO-SMR/UNICADO-SMR-180-TF/UNICADO-SMR-180-TF.xml b/docs/get-involved/modularization/python-template/projects/UNICADO-SMR/UNICADO-SMR-180-TF/UNICADO-SMR-180-TF.xml
new file mode 100644
index 0000000000000000000000000000000000000000..9a5c4dec713542fa19356c6a537d3b5c9ea6b7f0
--- /dev/null
+++ b/docs/get-involved/modularization/python-template/projects/UNICADO-SMR/UNICADO-SMR-180-TF/UNICADO-SMR-180-TF.xml
@@ -0,0 +1,10047 @@
+<aircraft_exchange_file>
+    <requirements_and_specifications description="Requirements and specifications">
+        <general description="General aircraft information">
+            <type description="Aircraft type">
+                <value>UNICADO</value>
+            </type>
+            <model description="Model - Version">
+                <value>SMR-180-TF</value>
+            </model>
+        </general>
+        <mission_files description="Name of xml files which are located in the mission_data directory and contain the flight phase data" tool_level="0">
+            <design_mission_file description="Name of the design mission xml">
+                <value>design_mission.xml</value>
+            </design_mission_file>
+            <study_mission_file description="Name of the study mission xml">
+                <value>study_mission.xml</value>
+            </study_mission_file>
+            <requirements_mission_file description="Name of the  requirements mission xml">
+                <value>requirements_mission.xml</value>
+            </requirements_mission_file>
+        </mission_files>
+        <design_specification description="Design specification">
+            <configuration description="Configuration information">
+                <configuration_type description="Aircraft configuration. Selector: tube_and_wing">
+                    <value>tube_and_wing</value>
+                </configuration_type>
+                <fuselage_definition description="Design description of the fuselage.">
+                    <fuselage_type description="Fuselage type. Selector: single_aisle / wide_body">
+                        <value>single_aisle</value>
+                    </fuselage_type>
+                    <fuselage_pressurization description="Switch to enable pressurized fuselage. Switch: true (On) / false (Off)">
+                        <value>true</value>
+                    </fuselage_pressurization>
+                </fuselage_definition>
+                <wing_definition description="Definitions for wing design">
+                    <mounting description="Wing mounting. Selector: low">
+                        <value>low</value>
+                    </mounting>
+                </wing_definition>
+                <empennage_definition description="Definitions for empennage design">
+                    <empennage_type description="Empennage type. Selector: conventional">
+                        <value>conventional</value>
+                    </empennage_type>
+                </empennage_definition>
+                <undercarriage_definition description="Design description of the undercarriage.">
+                    <main_gear_mounting description="Mounting position of the main landing gear. Selector: wing_mounted">
+                        <value>wing_mounted</value>
+                    </main_gear_mounting>
+                    <undercarriage_retractability description="Set retractability of landing gear. Selector: retractable / non_retractable">
+                        <value>retractable</value>
+                    </undercarriage_retractability>
+                </undercarriage_definition>
+                <tank_definition description="Energy tanks information">
+                    <tank ID="0" description="Inner left tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located. Selector: fuselage / wing / horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
+                            <value>inner_left</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="1" description="Outer left tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
+                            <value>outer_left</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="2" description="Inner right tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
+                            <value>inner_right</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="3" description="Outer right tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
+                            <value>outer_right</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="4" description="Center wing tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
+                            <value>center</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                </tank_definition>
+                <loads description="Loads information">
+                    <design_load_factor description="Design load factor n">
+                        <maximum description="Maximum design load factor n">
+                            <value>2.5</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>4</upper_boundary>
+                        </maximum>
+                        <minimum description="Minimum design load factor n">
+                            <value>-1.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>-2.0</lower_boundary>
+                            <upper_boundary>0.0</upper_boundary>
+                        </minimum>
+                        <maneuver description="Standard maneuver load factor for e.g. flare">
+                            <value>1.1</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>2.0</upper_boundary>
+                        </maneuver>
+                    </design_load_factor>
+                </loads>
+                <aerodynamic_technologies description="Integration of aerodynamic technologies on the aircraft: Switch: false (no additional aerodynamic technologies are considered)">
+                    <value>false</value>
+                </aerodynamic_technologies>
+            </configuration>
+            <transport_task description="Define the transport task for aircraft project.">
+                <passenger_definition description="Define the masses of the passengers">
+                    <total_number_passengers description="Design number of passengers">
+                        <value>180</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1000</upper_boundary>
+                    </total_number_passengers>
+                    <mass_per_passenger description="Design mass of a single passenger WITHOUT luggage">
+                        <value>80</value>
+                        <unit>kg</unit>
+                        <lower_boundary>50</lower_boundary>
+                        <upper_boundary>200</upper_boundary>
+                    </mass_per_passenger>
+                    <luggage_mass_per_passenger description="Design mass of the luggage for a single passenger">
+                        <value>15</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>25</upper_boundary>
+                    </luggage_mass_per_passenger>
+                </passenger_definition>
+                <multi_passenger_deck_layout description="Switch to select a multi passenger deck fuselage design. Switch: false (Off)">
+                    <value>false</value>
+                    <default>false</default>
+                    <specific_number_of_passenger_decks>
+                        <value>2</value>
+                        <unit>-</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>3</upper_boundary>
+                        <default>2</default>
+                    </specific_number_of_passenger_decks>
+                </multi_passenger_deck_layout>
+                <passenger_class_definition>
+                    <class_distribution description="Relative passenger distribution for the classes: President Class/First Class/Business Class/Premium Economy/Economy. Sum must be equal to 1!">
+                        <value>0/0/0/0/1</value>
+                    </class_distribution>
+                </passenger_class_definition>
+                <cargo_definition description="Definition of cargo which does not belong to passengers">
+                    <additional_cargo_mass description="Mass of cargo which does not belong to passengers">
+                        <value>2200</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>25000</upper_boundary>
+                    </additional_cargo_mass>
+                    <cargo_density description="Density of cargo which does not belong to passengers">
+                        <value>165</value>
+                        <unit>kg/m^3</unit>
+                        <lower_boundary>150</lower_boundary>
+                        <upper_boundary>200</upper_boundary>
+                    </cargo_density>
+                </cargo_definition>
+            </transport_task>
+            <energy_carriers description="Energy carriers information">
+                <energy_carrier ID="0" description="One specific energy carrier">
+                    <type description="Energy type (for multifuel engine create new ID). Selector: kerosene">
+                        <value>kerosene</value>
+                    </type>
+                    <density description="Energy carrier density.">
+                        <value>785</value>
+                        <unit>kg/m^3</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>10000</upper_boundary>
+                    </density>
+                </energy_carrier>
+            </energy_carriers>
+            <propulsion description="Propulsion information">
+                <propulsor ID="0" description="Information for specific propulsor">
+                    <powertrain description="Way the power is generated from the source. Selector: turbo">
+                        <value>turbo</value>
+                    </powertrain>
+                    <type description="Type of main thrust generator. Selector: fan">
+                        <value>fan</value>
+                    </type>
+                    <position description="Propulsor position (arrangement order acc to ID order)">
+                        <parent_component description="Position on component. Selector: wing / fuselage / empennage">
+                            <value>wing</value>
+                        </parent_component>
+                        <x description="X-position (aircraft coordinate system). Selector: front / back">
+                            <value>front</value>
+                        </x>
+                        <y description="Y-position (aircraft coordinate system). Selector: left / right">
+                            <value>left</value>
+                        </y>
+                        <z description="Z-position (aircraft coordinate system). Selector: over / mid / under / in">
+                            <value>under</value>
+                        </z>
+                    </position>
+                    <energy_carrier_ID description="See energy carrier specification node">
+                        <value>0</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </energy_carrier_ID>
+                    <thrust_share description="Share of this thrust in relation to required aircraft thrust">
+                        <value>0.5</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </thrust_share>
+                </propulsor>
+                <propulsor ID="1" description="Information for specific propulsor">
+                    <powertrain description="Way the power is generated from the source. Selector: turbo">
+                        <value>turbo</value>
+                    </powertrain>
+                    <type description="Type of main thrust generator. Selector: fan">
+                        <value>fan</value>
+                    </type>
+                    <position description="Propulsor position (arrangement order acc to ID order)">
+                        <parent_component description="Position on component. Selector: wing / fuselage / empennage">
+                            <value>wing</value>
+                        </parent_component>
+                        <x description="X-position (aircraft coordinate system). Selector: front / back">
+                            <value>front</value>
+                        </x>
+                        <y description="Y-position (aircraft coordinate system). Selector: left / right">
+                            <value>right</value>
+                        </y>
+                        <z description="Z-position (aircraft coordinate system). Selector: over / mid / under / in">
+                            <value>under</value>
+                        </z>
+                    </position>
+                    <energy_carrier_ID description="See energy carrier specification node">
+                        <value>0</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </energy_carrier_ID>
+                    <thrust_share description="Share of this thrust in relation to required aircraft thrust">
+                        <value>0.5</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </thrust_share>
+                </propulsor>
+                <energy_provider description="Source where energy is coming from per segment">
+                    <ground description="Source where energy is coming from in the ground mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </ground>
+                    <taxi description="source where energy is coming from in the taxi mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi>
+                    <takeoff description="source where energy is coming from in the takeoff mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </takeoff>
+                    <climb description="source where energy is coming from in the climb mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </climb>
+                    <cruise description="source where energy is coming from in the cruise mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </cruise>
+                    <descent description="source where energy is coming from in the descent mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </descent>
+                    <landing description="source where energy is coming from in the landing mission segment">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </landing>
+                </energy_provider>
+            </propulsion>
+            <technology>
+                <variable_camber description="Switch if variable camber is used. Switch: false (Off)">
+                    <value>false</value>
+                </variable_camber>
+            </technology>
+        </design_specification>
+        <requirements description="Aircraft design requirements">
+            <top_level_aircraft_requirements description="Top level aircraft requirements (TLAR)">
+                <maximum_structrual_payload_mass description="Maximum payload mass which can be carried by the aircraft (e.g. for short trips)">
+                    <value>19300</value>
+                    <unit>kg</unit>
+                    <lower_boundary>100</lower_boundary>
+                    <upper_boundary>150000</upper_boundary>
+                </maximum_structrual_payload_mass>
+                <takeoff_distance description="Design takeoff distance (Balanced Field Length) at Sea Level with maximum takeoff mass (MTOM) and (ISA + deltaISA)-Conditions">
+                    <value>1951</value>
+                    <unit>m</unit>
+                    <lower_boundary>600</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </takeoff_distance>
+                <landing_field_length description="Needed runway length at Sea Level with maximum landing mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)">
+                    <value>2425.67</value>
+                    <unit>m</unit>
+                    <lower_boundary>600</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </landing_field_length>
+                <icao_aerodrome_reference_code description="ICAO reference code - code_number 1-4 (field length) + code_letter A-F (wing span limits) + faa ADG code number I-VI (wing span limits + tail height limits) + Aircraft Approach Category letter  A-D">
+                    <value>3CIIIC</value>
+                </icao_aerodrome_reference_code>
+                <flight_envelope description="Maxima of design flight envelope">
+                    <maximum_operating_mach_number description="Maximum operating mach number">
+                        <value>0.82</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </maximum_operating_mach_number>
+                    <maximum_operating_velocity description="Maximum operating speed (maximum dynamic pressure)">
+                        <value>180</value>
+                        <unit>m/s</unit>
+                        <lower_boundary>50</lower_boundary>
+                        <upper_boundary>250</upper_boundary>
+                    </maximum_operating_velocity>
+                    <maximum_approach_speed description="Maximum allowed approach speed.">
+                        <value>67.65</value>
+                        <unit>m/s</unit>
+                        <lower_boundary>50</lower_boundary>
+                        <upper_boundary>90</upper_boundary>
+                    </maximum_approach_speed>
+                    <maximum_operating_altitude description="Maximum operating altitude">
+                        <value>12192</value>
+                        <unit>m</unit>
+                        <lower_boundary>4500</lower_boundary>
+                        <upper_boundary>20000</upper_boundary>
+                    </maximum_operating_altitude>
+                    <maximum_altitude_one_engine_inoperative description="Maximum operating altitude with one engine inoperative">
+                        <value>4572</value>
+                        <unit>m</unit>
+                        <lower_boundary>1500</lower_boundary>
+                        <upper_boundary>12000</upper_boundary>
+                    </maximum_altitude_one_engine_inoperative>
+                    <climb_or_descent_segment_gradient description="climb / descent segment gradient">
+                        <value>0.024</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </climb_or_descent_segment_gradient>
+                </flight_envelope>
+                <pavement_classification_number description="Runway pavement classification number (PCN) - limits the maximum allowed aircraft classification number of undercarriage">
+                    <value>55</value>
+                    <unit>1</unit>
+                    <lower_boundary>5</lower_boundary>
+                    <upper_boundary>120</upper_boundary>
+                </pavement_classification_number>
+                <design_mission description="Requirements regarding the design mission">
+                    <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
+                        <value>0</value>
+                        <unit>K</unit>
+                        <lower_boundary>-100</lower_boundary>
+                        <upper_boundary>100</upper_boundary>
+                    </delta_ISA>
+                    <range description="Target range for design mission">
+                        <value>4537400</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>20000000</upper_boundary>
+                    </range>
+                    <contingency description="Contingency fuel in percentage (reserve fuel)">
+                        <value>0.06</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>0.08</upper_boundary>
+                    </contingency>
+                    <alt_dist description="Alternate distance in m (reserve fuel)">
+                        <value>370400</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>926000</upper_boundary>
+                    </alt_dist>
+                    <loiter_time description="Loiter time in seconds (reserve fuel)">
+                        <value>1800</value>
+                        <unit>s</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>3600</upper_boundary>
+                    </loiter_time>
+                    <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise">
+                        <value>0.78</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </initial_cruise_mach_number>
+                    <initial_cruise_altitude description="Initial cruise altitude (ICA) at top of descent. May be altered during cruise">
+                        <value>10058.4</value>
+                        <unit>m</unit>
+                        <lower_boundary>1000</lower_boundary>
+                        <upper_boundary>20000</upper_boundary>
+                    </initial_cruise_altitude>
+                    <climb_speed_schedule description="Climb speed for different altitudes">
+                        <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_below_FL100>
+                        <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_above_FL100>
+                        <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
+                            <value>-0.02</value>
+                            <unit>1</unit>
+                            <lower_boundary>-0.3</lower_boundary>
+                            <upper_boundary>0.01</upper_boundary>
+                        </delta_mach_climb_cruise>
+                    </climb_speed_schedule>
+                    <descent_speed_schedule description="Descent speed for different altitudes">
+                        <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_below_FL100>
+                        <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_above_FL100>
+                    </descent_speed_schedule>
+                    <time_to_climb description="Time the aircraft takes to climb to cruise altitude">
+                        <value>2100</value>
+                        <unit>s</unit>
+                        <lower_boundary>600</lower_boundary>
+                        <upper_boundary>3600</upper_boundary>
+                    </time_to_climb>
+                    <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+                        <fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)">
+                            <value>mode_0</value>
+                        </fuel_estimation_selector>
+                    </fuel_planning>
+                </design_mission>
+                <study_mission description="Requirements regarding the study mission">
+                    <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
+                        <value>0</value>
+                        <unit>K</unit>
+                        <lower_boundary>-100</lower_boundary>
+                        <upper_boundary>100</upper_boundary>
+                    </delta_ISA>
+                    <range description="Target range for the study mission">
+                        <value>1481600</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>20000000</upper_boundary>
+                    </range>
+                    <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise">
+                        <value>0.78</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </initial_cruise_mach_number>
+                    <initial_cruise_altitude description="Initial cruise altitude at top of descent. May be altered during cruise">
+                        <value>10668</value>
+                        <unit>m</unit>
+                        <lower_boundary>1000</lower_boundary>
+                        <upper_boundary>20000</upper_boundary>
+                    </initial_cruise_altitude>
+                    <climb_speed_schedule description="Climb speed for different altitudes">
+                        <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_below_FL100>
+                        <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_above_FL100>
+                        <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
+                            <value>-0.02</value>
+                            <unit>1</unit>
+                            <lower_boundary>-0.3</lower_boundary>
+                            <upper_boundary>0.01</upper_boundary>
+                        </delta_mach_climb_cruise>
+                    </climb_speed_schedule>
+                    <descent_speed_schedule description="Descent speed for different altitudes">
+                        <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_below_FL100>
+                        <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_above_FL100>
+                    </descent_speed_schedule>
+                    <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+                        <fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)">
+                            <value>mode_0</value>
+                        </fuel_estimation_selector>
+                    </fuel_planning>
+                    <payload_fractions description="Set the fraction of different design payload values for the study mission">
+                        <cargo_fraction description="Fraction of the design cargo mass which is used for the study mission">
+                            <value>0.75</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </cargo_fraction>
+                        <passenger_mass_fraction description="Fraction of the design passenger mass which is used for the study mission">
+                            <value>0.75</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </passenger_mass_fraction>
+                    </payload_fractions>
+                </study_mission>
+            </top_level_aircraft_requirements>
+            <additional_requirements description="Additional requirements">
+                <landing_gear description="Landing gear requirements and operational conditions">
+                    <friction_coefficient description="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">
+                        <value>0.03</value>
+                        <default>0.03</default>
+                        <unit>1</unit>
+                        <lower_boundary>0.02</lower_boundary>
+                        <upper_boundary>0.08</upper_boundary>
+                    </friction_coefficient>
+                    <braking_coefficient description="Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189">
+                        <value>0.34189</value>
+                        <default>0.34189</default>
+                        <unit>1</unit>
+                        <lower_boundary>0.06</lower_boundary>
+                        <upper_boundary>0.5</upper_boundary>
+                    </braking_coefficient>
+                </landing_gear>
+            </additional_requirements>
+        </requirements>
+        <assessment_scenario description="Scenario for ecological and economical assessment">
+            <flights_per_year description="Number of flights per year">
+                <value>2227</value>
+                <unit>1</unit>
+                <lower_boundary>0</lower_boundary>
+                <upper_boundary>4000</upper_boundary>
+            </flights_per_year>
+            <duration_operation description="Operating years of aircraft">
+                <value>25</value>
+                <unit>a</unit>
+                <lower_boundary>0</lower_boundary>
+                <upper_boundary>50</upper_boundary>
+            </duration_operation>
+        </assessment_scenario>
+    </requirements_and_specifications>
+    <analysis>
+        <masses_cg_inertia description="Masses, Center of Gravity, Inertias." tool_level="3">
+            <maximum_takeoff_mass description="MTOM">
+                <mass_properties description="maximum takeoff mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1516369.8991</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3734413.0755</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>5298372.6073</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.1407</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.489</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>78910.0176</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_takeoff_mass>
+            <operating_mass_empty description="OME">
+                <mass_properties description="operating mass empty properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>858287.8112</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>2113733.0848</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>2998957.3326</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>14.6479</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.7597</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>44664.2382</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </operating_mass_empty>
+            <manufacturer_mass_empty description="MME">
+                <mass_properties description="manufacturer mass empty properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>778817.1694</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>1918018.1712</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>2721277.6769</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>14.5122</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.8372</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>40528.6841</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </manufacturer_mass_empty>
+            <maximum_zero_fuel_mass description="MZFM">
+                <mass_properties description="maximum zero fuel mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1229165.1716</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3027104.7266</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>4294845.9205</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.3016</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.6033</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>63964.2382</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_zero_fuel_mass>
+            <maximum_payload_mass description="">
+                <mass_properties description="maximum payload mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>16.8143</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.2413</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>19300</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_payload_mass>
+            <maximum_landing_mass description="MLM">
+                <mass_properties description="maximum landing mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1278687.6683</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3149065.3769</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>4467883.2775</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>14.6479</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.7597</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>66541.3278</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_landing_mass>
+            <maximum_fuel_mass description="">
+                <mass_properties description="maximum fuel mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>14.5199</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>16477.4718</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_fuel_mass>
+            <ferry_range_mass description="">
+                <mass_properties description="ferry range mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>14.6134</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.5549</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>61141.7099</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </ferry_range_mass>
+            <most_forward_mass description="">
+                <mass_properties description="most forward mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>858287.8112</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>2113733.0848</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>2998957.3326</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>14.217</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>64890.0176</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </most_forward_mass>
+            <most_afterward_mass description="">
+                <mass_properties description="most afterward mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>858287.8112</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>2113733.0848</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>2998957.3326</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.4886</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>67770.0176</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </most_afterward_mass>
+            <design_mass description="">
+                <mass_properties description="design mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1516369.8991</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3734413.0755</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>5298372.6073</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.1407</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.489</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>78910.0176</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </design_mass>
+            <design_fuel_mass description="">
+                <mass_properties description="design fuel mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>14.4524</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>14945.7795</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </design_fuel_mass>
+        </masses_cg_inertia>
+        <aerodynamics description="Aerodynamical analysis" tool_level="3">
+            <polar>
+                <polar_file description="Name of polar file">
+                    <value>SMR-180-TF_design_trimmed_polar.xml</value>
+                </polar_file>
+                <configurations description="Number of configurations in the polar file">
+                    <value>7</value>
+                    <unit>1</unit>
+                    <lower_boundary>-2147483648</lower_boundary>
+                    <upper_boundary>2147483647</upper_boundary>
+                </configurations>
+                <configuration ID="0" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>cruise</value>
+                    </type>
+                    <name description=" Name">
+                        <value>clean</value>
+                    </name>
+                </configuration>
+                <configuration ID="1" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>departure</value>
+                    </type>
+                    <name description=" Name">
+                        <value>takeoff</value>
+                    </name>
+                </configuration>
+                <configuration ID="2" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>departure</value>
+                    </type>
+                    <name description=" Name">
+                        <value>takeoff_landing_gear_retracted</value>
+                    </name>
+                </configuration>
+                <configuration ID="3" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>departure</value>
+                    </type>
+                    <name description=" Name">
+                        <value>climb</value>
+                    </name>
+                </configuration>
+                <configuration ID="4" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>approach</value>
+                    </type>
+                    <name description=" Name">
+                        <value>approach</value>
+                    </name>
+                </configuration>
+                <configuration ID="5" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>approach</value>
+                    </type>
+                    <name description=" Name">
+                        <value>approach_landing_gear_out</value>
+                    </name>
+                </configuration>
+                <configuration ID="6" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>approach</value>
+                    </type>
+                    <name description=" Name">
+                        <value>landing</value>
+                    </name>
+                </configuration>
+            </polar>
+            <reference_values>
+                <b description="Wing half span">
+                    <value>35.54591898</value>
+                    <unit>m</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </b>
+                <MAC description="Mean aerodynamic chord">
+                    <value>4.471119328</value>
+                    <unit>m</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </MAC>
+                <S_ref description="Wing reference area">
+                    <value>133.0013007</value>
+                    <unit>m^2</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </S_ref>
+                <neutral_point>
+                    <x description="x component of neutral point">
+                        <value>16.45886264</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </x>
+                </neutral_point>
+            </reference_values>
+            <lift_coefficients>
+                <C_LoptimumCruise description="C_LoptimumCruise">
+                    <value>0.62</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LoptimumCruise>
+                <C_LmaxLanding description="C_LmaxLanding">
+                    <value>3.135</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LmaxLanding>
+                <C_LmaxT-O description="C_LmaxTO">
+                    <value>2.681</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LmaxT-O>
+                <C_LgroundRoll description="C_LgroundRoll">
+                    <value>0.4</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LgroundRoll>
+            </lift_coefficients>
+            <max_spoiler_factor description="max_spoiler_factor">
+                <value>2.5</value>
+                <unit>1</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </max_spoiler_factor>
+        </aerodynamics>
+        <mission description="Mission data" tool_level="0">
+            <design_mission description="Data of design mission">
+                <range description="Traveled range from break release to end of taxi at destination">
+                    <value>4538395.775</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>20000000</upper_boundary>
+                </range>
+                <loaded_mission_energy description="Amount of energy loaded into tanks (including reserves) for the mission">
+                    <mission_energy ID="0" description="Amount of energy loaded into tanks (including reserves) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>6.579765969e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </mission_energy>
+                </loaded_mission_energy>
+                <in_flight_energy description="Amount of energy needed for in-flight segments (all segments from takeoff to landing)">
+                    <trip_energy ID="0" description="Amount of energy needed for trip segments (all segments from takeoff to landing) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>5.2160675e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </trip_energy>
+                    <takeoff_energy ID="0" description="Amount of energy needed for takeoff segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>9450750027</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </takeoff_energy>
+                    <landing_energy ID="0" description="Amount of energy needed for landing segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>6656167607</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </landing_energy>
+                </in_flight_energy>
+                <taxi_energy description="Amount of energy needed for taxiing specified energy carrier">
+                    <taxi_out_energy ID="0" description="Amount of energy needed for taxiing at origin for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>1.381350162e+10</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_out_energy>
+                    <taxi_in_energy ID="0" description="Amount of energy needed for taxiing at destination for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7674167565</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_in_energy>
+                </taxi_energy>
+                <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
+                    <value>21026.71256</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>45000</upper_boundary>
+                </block_time>
+                <flight_time description="Flight time for the whole mission">
+                    <value>20186.71256</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>44500</upper_boundary>
+                </flight_time>
+                <takeoff_engine_derate description="Engine power demand">
+                    <value>1</value>
+                    <unit>1</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1</upper_boundary>
+                </takeoff_engine_derate>
+                <cruise description="Characteristics of the cruise segment">
+                    <average_lift_coefficient description="Lift coefficient CL_average: Arithmetic mean over the entire cruise flight">
+                        <value>0.5004788333</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </average_lift_coefficient>
+                    <minimum_lift_coefficient description="Minimum cruise flight lift coefficient CL_min">
+                        <value>0.4779122031</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </minimum_lift_coefficient>
+                    <maximum_lift_coefficient description="Maximum cruise flight lift coefficient CL_max">
+                        <value>0.539875665</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </maximum_lift_coefficient>
+                    <top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
+                        <value>77580.69965</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_climb_mass>
+                    <top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
+                        <value>67345.98464</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_descent_mass>
+                    <top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
+                        <value>209304.6152</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>4537400</upper_boundary>
+                    </top_of_climb_range>
+                    <top_of_descent_range description="Flown range from takeoff to top of descent">
+                        <value>4320705.697</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>4537400</upper_boundary>
+                    </top_of_descent_range>
+                    <cruise_steps description="Cruise step information">
+                        <cruise_step ID="0" description="Data of a cruise step">
+                            <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+                                <value>0.4992815941</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </relative_end_of_cruise_step>
+                            <altitude description="Altitude of cruise step">
+                                <value>10058.40002</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>15000</upper_boundary>
+                            </altitude>
+                        </cruise_step>
+                        <cruise_step ID="1" description="Data of a cruise step">
+                            <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </relative_end_of_cruise_step>
+                            <altitude description="Altitude of cruise step">
+                                <value>10668.00002</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>15000</upper_boundary>
+                            </altitude>
+                        </cruise_step>
+                    </cruise_steps>
+                </cruise>
+            </design_mission>
+            <study_mission description="Data of study mission">
+                <takeoff_mass description="Takeoff mass">
+                    <value>65647.30948</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>300000</upper_boundary>
+                </takeoff_mass>
+                <range description="Traveled range from break release to end of taxi at destination">
+                    <value>1482610.029</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>20000000</upper_boundary>
+                </range>
+                <loaded_mission_energy description="Amount of energy loaded into tanks (including reserves) for the mission">
+                    <mission_energy ID="0" description="Amount of energy loaded into tanks (including reserves) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>2.938291892e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </mission_energy>
+                </loaded_mission_energy>
+                <in_flight_energy description="Amount of energy needed for in-flight segments (all segments from takeoff to landing)">
+                    <trip_energy ID="0" description="Amount of energy needed for trip segments (all segments from takeoff to landing) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>1.705162335e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </trip_energy>
+                    <takeoff_energy ID="0" description="Amount of energy needed for takeoff segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7302361823</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </takeoff_energy>
+                    <landing_energy ID="0" description="Amount of energy needed for landing segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7674271840</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </landing_energy>
+                </in_flight_energy>
+                <taxi_energy description="Amount of energy needed for taxiing specified energy carrier">
+                    <taxi_out_energy ID="0" description="Amount of energy needed for taxiing at origin for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>1.333131716e+10</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_out_energy>
+                    <taxi_in_energy ID="0" description="Amount of energy needed for taxiing at destination for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7406287311</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+13</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_in_energy>
+                </taxi_energy>
+                <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
+                    <value>7843.969995</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>45000</upper_boundary>
+                </block_time>
+                <flight_time description="Flight time for the whole mission">
+                    <value>7003.969995</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>44500</upper_boundary>
+                </flight_time>
+                <takeoff_engine_derate description="Engine power demand">
+                    <value>1</value>
+                    <unit>1</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1</upper_boundary>
+                </takeoff_engine_derate>
+                <cruise description="Characteristics of the cruise segment">
+                    <average_lift_coefficient description="Lift coefficient CL_average: Arithmetic mean over the entire cruise flight">
+                        <value>0.45750799</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </average_lift_coefficient>
+                    <minimum_lift_coefficient description="Minimum cruise flight lift coefficient CL_min">
+                        <value>0.448770596</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </minimum_lift_coefficient>
+                    <maximum_lift_coefficient description="Maximum cruise flight lift coefficient CL_max">
+                        <value>0.4909341943</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </maximum_lift_coefficient>
+                    <top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
+                        <value>64207.94954</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_climb_mass>
+                    <top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
+                        <value>61801.39938</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_descent_mass>
+                    <top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
+                        <value>173868.7843</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>4537400</upper_boundary>
+                    </top_of_climb_range>
+                    <top_of_descent_range description="Flown range from takeoff to top of descent">
+                        <value>1271751.648</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>4537400</upper_boundary>
+                    </top_of_descent_range>
+                    <cruise_steps description="Cruise step information">
+                        <cruise_step ID="0" description="Data of a cruise step">
+                            <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </relative_end_of_cruise_step>
+                            <altitude description="Altitude of cruise step">
+                                <value>10668.00002</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>15000</upper_boundary>
+                            </altitude>
+                        </cruise_step>
+                    </cruise_steps>
+                </cruise>
+            </study_mission>
+        </mission>
+    </analysis>
+    <component_design>
+        <global_reference_point>
+            <reference_component description="Global reference point of aircraft geometry">
+                <value>fuselage</value>
+            </reference_component>
+            <x description="X coordinate of the global reference point">
+                <value>0</value>
+                <unit>m</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </x>
+            <y description="Y coordinate of the global reference point">
+                <value>0</value>
+                <unit>m</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </y>
+            <z description="Z coordinate of the global reference point">
+                <value>0</value>
+                <unit>m</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </z>
+        </global_reference_point>
+        <wing>
+            <mass_properties description="mass_properties of component wing">
+                <mass description="component mass">
+                    <value>8274.774993</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="component inertia referred to local center of gravity">
+                    <j_xx description="wing inertia in x">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="wing inertia in y">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="wing inertia in z">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="wing inertia in xy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="wing inertia in xz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="wing inertia in yx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="wing inertia in yz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="wing inertia in zx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="wing inertia in zy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                    <x description="x position of center of gravity">
+                        <value>15.54656757</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </x>
+                    <y description="y position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </y>
+                    <z description="z position of center of gravity">
+                        <value>-0.705331188</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <position description="position of wing">
+                <x description="x position">
+                    <value>11.39593946</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </x>
+                <y description="y position">
+                    <value>0</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </y>
+                <z description="z position">
+                    <value>-1.030571436</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </z>
+            </position>
+            <specific>
+                <geometry>
+                    <aerodynamic_surface ID="0" description="main_wing">
+                        <name description="name of surface">
+                            <value>main_wing</value>
+                        </name>
+                        <position description="reference position in aircraft coordinates">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <parameters description="aerodynamic surface parameters">
+                            <direction description="unit vector according to aircraft coordinate system for direction applied at position">
+                                <x description="x direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y direction of unit vector">
+                                    <value>-1</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </direction>
+                            <symmetric description="symmetric to local x-z plane">
+                                <value>true</value>
+                            </symmetric>
+                            <sections description="sections">
+                                <section ID="0">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>6.430370554</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1.00040016</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                                <section ID="1">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-1.983993414</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>6.430370554</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1.00040016</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                                <section ID="2">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>2.023046511</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0.2341075845</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-5.331887848</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>4.582779756</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>0.9169761572</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                                <section ID="3">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>8.696817677</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>1.104072062</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-17.77295949</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>1.093162994</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>0.6069651886</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                            </sections>
+                            <spars>
+                                <spar ID="0" description="front_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                                <spar ID="1" description="rear_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                            </spars>
+                            <control_devices>
+                                <control_device ID="0" description="slat">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.1138624821</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.294</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.6981317008</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="1" description="slat">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.306</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.95</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.6981317008</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="2" description="flap_fowler">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.1138624821</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.297</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="3" description="flap_fowler">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.303</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.78</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="4" description="aileron">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.8</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.98</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>-0.3490658504</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.3490658504</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="5" description="spoiler_ground">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.2039312411</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.294</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="6" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.306</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.4195</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="7" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.4195</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.533</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="8" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.533</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.6465</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="9" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.6465</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.76</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                            </control_devices>
+                        </parameters>
+                    </aerodynamic_surface>
+                </geometry>
+            </specific>
+        </wing>
+        <empennage>
+            <position description="position of empennage">
+                <x description="x position">
+                    <value>30.56333685</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </x>
+                <y description="y position">
+                    <value>0</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </y>
+                <z description="z position">
+                    <value>0.92429206</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="mass_properties of component Conventional tail overall mass">
+                <mass description="component mass">
+                    <value>1004.750174</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="component inertia referred to local center of gravity">
+                    <j_xx description="Conventional tail overall mass inertia in x">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Conventional tail overall mass inertia in y">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Conventional tail overall mass inertia in z">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Conventional tail overall mass inertia in xy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Conventional tail overall mass inertia in xz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Conventional tail overall mass inertia in yx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Conventional tail overall mass inertia in yz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Conventional tail overall mass inertia in zx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Conventional tail overall mass inertia in zy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                    <x description="x position of center of gravity">
+                        <value>34.53808851</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </x>
+                    <y description="y position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </y>
+                    <z description="z position of center of gravity">
+                        <value>2.994918735</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific>
+                <geometry>
+                    <aerodynamic_surface ID="0" description="vertical_stabiliser">
+                        <name description="name of surface">
+                            <value>vertical_stabiliser</value>
+                        </name>
+                        <position description="reference position in aircraft coordinates">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <parameters description="aerodynamic surface parameters">
+                            <direction description="unit vector according to aircraft coordinate system for direction applied at position">
+                                <x description="x direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z direction of unit vector">
+                                    <value>-1</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </direction>
+                            <symmetric description="symmetric to local x-z plane">
+                                <value>false</value>
+                            </symmetric>
+                            <sections description="sections">
+                                <section ID="0">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>5.22784579</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                                <section ID="1">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>4.734999795</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-6.283556967</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>1.386424703</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                            </sections>
+                            <spars>
+                                <spar ID="0" description="front_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                                <spar ID="1" description="rear_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                            </spars>
+                            <control_devices>
+                                <control_device ID="0" description="rudder">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.9</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>-0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                            </control_devices>
+                        </parameters>
+                        <mass_properties description="mass_properties of component vertical stabiliser mass">
+                            <mass description="component mass">
+                                <value>412.1612023</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </mass>
+                            <inertia description="component inertia referred to local center of gravity">
+                                <j_xx description="vertical stabiliser mass inertia in x">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="vertical stabiliser mass inertia in y">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="vertical stabiliser mass inertia in z">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="vertical stabiliser mass inertia in xy">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="vertical stabiliser mass inertia in xz">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="vertical stabiliser mass inertia in yx">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="vertical stabiliser mass inertia in yz">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="vertical stabiliser mass inertia in zx">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="vertical stabiliser mass inertia in zy">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                                <x description="x position of center of gravity">
+                                    <value>33.76014602</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y position of center of gravity">
+                                    <value>0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z position of center of gravity">
+                                    <value>3.457845538</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </aerodynamic_surface>
+                    <aerodynamic_surface ID="1" description="horizontal_stabiliser">
+                        <name description="name of surface">
+                            <value>horizontal_stabiliser</value>
+                        </name>
+                        <position description="reference position in aircraft coordinates">
+                            <x description="x coordinate of point">
+                                <value>2.169576111</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>-0.5869856587</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <parameters description="aerodynamic surface parameters">
+                            <direction description="unit vector according to aircraft coordinate system for direction applied at position">
+                                <x description="x direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y direction of unit vector">
+                                    <value>-1</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </direction>
+                            <symmetric description="symmetric to local x-z plane">
+                                <value>true</value>
+                            </symmetric>
+                            <sections description="sections">
+                                <section ID="0">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>3.558269679</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                                <section ID="1">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>3.315686706</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0.4015853348</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-5.742937844</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>1.004143703</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                            </sections>
+                            <spars>
+                                <spar ID="0" description="front_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                                <spar ID="1" description="rear_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                            </spars>
+                            <control_devices>
+                                <control_device ID="0" description="elevator">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.2</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.9</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>-0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                            </control_devices>
+                        </parameters>
+                        <mass_properties description="mass_properties of component horizontal stabiliser mass">
+                            <mass description="component mass">
+                                <value>592.5889713</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </mass>
+                            <inertia description="component inertia referred to local center of gravity">
+                                <j_xx description="horizontal stabiliser mass inertia in x">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="horizontal stabiliser mass inertia in y">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="horizontal stabiliser mass inertia in z">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="horizontal stabiliser mass inertia in xy">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="horizontal stabiliser mass inertia in xz">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="horizontal stabiliser mass inertia in yx">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="horizontal stabiliser mass inertia in yz">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="horizontal stabiliser mass inertia in zx">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="horizontal stabiliser mass inertia in zy">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                                <x description="x position of center of gravity">
+                                    <value>35.07916795</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y position of center of gravity">
+                                    <value>0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z position of center of gravity">
+                                    <value>2.672940978</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </aerodynamic_surface>
+                </geometry>
+            </specific>
+        </empennage>
+        <propulsion>
+            <position description="Reference position of the propulsion assembly">
+                <x description="x coordinate of point">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </x>
+                <y description="y coordinate of point">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </y>
+                <z description="z coordinate of point">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of the propulsion assembly">
+                <mass description="mass of the of the component">
+                    <value>9280.286214</value>
+                    <unit>kg</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of the component in respect to the CG">
+                    <j_xx description="inertia of the component">
+                        <value>366747.7055</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="inertia of the component">
+                        <value>15925.10007</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="inertia of the component">
+                        <value>373826.6302</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="inertia of the component">
+                        <value>-0.05485075752</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="inertia of the component">
+                        <value>3607.527674</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="inertia of the component">
+                        <value>-0.05485075752</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="inertia of the component">
+                        <value>-0.007574981387</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="inertia of the component">
+                        <value>3607.527674</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="inertia of the component">
+                        <value>-0.007574981387</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                    <x description="x coordinate of the center of gravity">
+                        <value>12.01324646</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </x>
+                    <y description="y coordinate of the center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </y>
+                    <z description="z coordinate of the center of gravity">
+                        <value>-2.360884877</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific>
+                <propulsion ID="0" description="Description of one propulsion">
+                    <nacelle ID="0" description="Nacelle of the propulsion assembly">
+                        <position description="Origin of the nacelle RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="Normal direction of the nacelle in the global aircraft coordinate system">
+                            <x description="x direction of unit vector">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="Geometrical description nacelle sections">
+                            <section ID="0">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.278846336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.278846336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0.8669835302</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.757404066</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.757404066</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="2">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>2.600950591</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.757404066</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.757404066</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="3">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>3.467934121</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.278846336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.278846336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the nacelle">
+                            <mass description="mass of the of the component">
+                                <value>1088.228779</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>50.50632457</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>53.03914847</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>53.04341794</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.0007846523573</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>-0.003274935904</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.0007846523573</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.0006083354311</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>-0.003274935904</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.0006083354311</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>11.73777819</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>-6.231052716</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.545347304</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </nacelle>
+                    <pylon ID="0" description="pylon of the propulsion assembly">
+                        <position description="Position of the pylon RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="unit vector according to aircraft coordinate system for direction applied at position">
+                            <x description="x direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>-1.139423168</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="sections">
+                            <section ID="0">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0.8669835302</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>1.688423032e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.378702033</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.467934121</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>3.897514364</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>2.218765086e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.811759185</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.467934121</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the pylon">
+                            <mass description="mass of the of the component">
+                                <value>536.5569409</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>0.1482730907</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>8.344815004</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>8.347745517</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.0266407264</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0.5059988459</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.0266407264</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.00317915525</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0.5059988459</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.00317915525</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>14.12002714</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>-6.231052716</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-0.9501166946</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </pylon>
+                    <engine>
+                        <model description="Name of selected engine model">
+                            <value>PW1127G-JM</value>
+                        </model>
+                        <position description="Position of the engine in the global coordinate system">
+                            <x description="x coordinate of point">
+                                <value>10.00381113</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>-6.231052716</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>-2.545347304</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of the engine">
+                            <mass description="mass of the of the component">
+                                <value>3015.357387</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>1957.396868</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>4000.731588</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>4000.731588</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>11.73777819</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>-6.231052716</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.545347304</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <SLST description="Sea level static thrust of the engine">
+                            <value>126361.2254</value>
+                            <unit>N</unit>
+                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </SLST>
+                        <scale_factor description="Scale factor of the engine">
+                            <value>1.049930415</value>
+                            <unit>1</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </scale_factor>
+                        <bucket_point description="Bucket point of the engine at initial cruise flight phase">
+                            <thrust description="Thrust of the engine at the bucket point">
+                                <value>20848.89859</value>
+                                <unit>N</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </thrust>
+                            <tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
+                                <value>1.503317406e-05</value>
+                                <unit>kg/Ns</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </tsfc>
+                        </bucket_point>
+                    </engine>
+                </propulsion>
+                <propulsion ID="1" description="Description of one propulsion">
+                    <nacelle ID="0" description="Nacelle of the propulsion assembly">
+                        <position description="Origin of the nacelle RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="Normal direction of the nacelle in the global aircraft coordinate system">
+                            <x description="x direction of unit vector">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="Geometrical description nacelle sections">
+                            <section ID="0">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.278846336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.278846336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0.8669835302</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.757404066</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.757404066</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="2">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>2.600950591</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.757404066</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.757404066</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="3">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>3.467934121</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.278846336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.278846336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the nacelle">
+                            <mass description="mass of the of the component">
+                                <value>1088.228779</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>50.50632457</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>53.03914847</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>53.04341794</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.0007846523573</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>-0.003274935904</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.0007846523573</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.0006083354311</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>-0.003274935904</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.0006083354311</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>11.73777819</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>6.231052716</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.545347304</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </nacelle>
+                    <pylon ID="0" description="pylon of the propulsion assembly">
+                        <position description="Position of the pylon RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="unit vector according to aircraft coordinate system for direction applied at position">
+                            <x description="x direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>-1.139423168</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="sections">
+                            <section ID="0">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0.8669835302</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>1.688423032e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.378702033</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.467934121</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>3.897514364</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>2.218765086e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.811759185</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.467934121</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the pylon">
+                            <mass description="mass of the of the component">
+                                <value>536.5569409</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>0.1482730907</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>8.344815004</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>8.347745517</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.0266407264</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0.5059988459</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.0266407264</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.00317915525</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0.5059988459</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.00317915525</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>14.12002714</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>6.231052716</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-0.9501166946</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </pylon>
+                    <engine>
+                        <model description="Name of selected engine model">
+                            <value>PW1127G-JM</value>
+                        </model>
+                        <position description="Position of the engine in the global coordinate system">
+                            <x description="x coordinate of point">
+                                <value>10.00381113</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>6.231052716</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>-2.545347304</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of the engine">
+                            <mass description="mass of the of the component">
+                                <value>3015.357387</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>1957.396868</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>4000.731588</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>4000.731588</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>11.73777819</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>6.231052716</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.545347304</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <SLST description="Sea level static thrust of the engine">
+                            <value>126361.2254</value>
+                            <unit>N</unit>
+                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </SLST>
+                        <scale_factor description="Scale factor of the engine">
+                            <value>1.049930415</value>
+                            <unit>1</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </scale_factor>
+                        <bucket_point description="Bucket point of the engine at initial cruise flight phase">
+                            <thrust description="Thrust of the engine at the bucket point">
+                                <value>20848.89859</value>
+                                <unit>N</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </thrust>
+                            <tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
+                                <value>1.503317406e-05</value>
+                                <unit>kg/Ns</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </tsfc>
+                        </bucket_point>
+                    </engine>
+                </propulsion>
+            </specific>
+        </propulsion>
+        <systems>
+            <mass_properties description="mass_properties of component systems">
+                <mass description="component mass">
+                    <value>6008.790861</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="component inertia referred to local center of gravity">
+                    <j_xx description="systems inertia in x">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="systems inertia in y">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="systems inertia in z">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="systems inertia in xy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="systems inertia in xz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="systems inertia in yx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="systems inertia in yz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="systems inertia in zx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="systems inertia in zy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                    <x description="x position of center of gravity">
+                        <value>7.973530556</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </x>
+                    <y description="y position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </y>
+                    <z description="z position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <operator_items>
+                <operator_item ID="0">
+                    <name description="name of the operator item">
+                        <value>water_and_toilet_chemicals</value>
+                    </name>
+                    <mass_properties description="mass_properties of component water and toilet chemicals">
+                        <mass description="component mass">
+                            <value>244.8</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </mass>
+                        <inertia description="component inertia referred to local center of gravity">
+                            <j_xx description="water and toilet chemicals inertia in x">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xx>
+                            <j_yy description="water and toilet chemicals inertia in y">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yy>
+                            <j_zz description="water and toilet chemicals inertia in z">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zz>
+                            <j_xy description="water and toilet chemicals inertia in xy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xy>
+                            <j_xz description="water and toilet chemicals inertia in xz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xz>
+                            <j_yx description="water and toilet chemicals inertia in yx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yx>
+                            <j_yz description="water and toilet chemicals inertia in yz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yz>
+                            <j_zx description="water and toilet chemicals inertia in zx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zx>
+                            <j_zy description="water and toilet chemicals inertia in zy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                            <x description="x position of center of gravity">
+                                <value>3.215185277</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                    </mass_properties>
+                </operator_item>
+                <operator_item ID="1">
+                    <name description="name of the operator item">
+                        <value>residual_oil_and_fuel</value>
+                    </name>
+                    <mass_properties description="mass_properties of component water and toilet chemicals">
+                        <mass description="component mass">
+                            <value>1.149011107</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </mass>
+                        <inertia description="component inertia referred to local center of gravity">
+                            <j_xx description="water and toilet chemicals inertia in x">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xx>
+                            <j_yy description="water and toilet chemicals inertia in y">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yy>
+                            <j_zz description="water and toilet chemicals inertia in z">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zz>
+                            <j_xy description="water and toilet chemicals inertia in xy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xy>
+                            <j_xz description="water and toilet chemicals inertia in xz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xz>
+                            <j_yx description="water and toilet chemicals inertia in yx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yx>
+                            <j_yz description="water and toilet chemicals inertia in yz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yz>
+                            <j_zx description="water and toilet chemicals inertia in zx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zx>
+                            <j_zy description="water and toilet chemicals inertia in zy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                            <x description="x position of center of gravity">
+                                <value>15.54656757</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                    </mass_properties>
+                </operator_item>
+            </operator_items>
+            <specific>
+                <geometry>
+                    <mass_properties>
+                        <fuel_system description="mass of ATA-28">
+                            <value>214.9196007</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </fuel_system>
+                        <de_icing description="mass of ATA-30">
+                            <value>44.7349324</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </de_icing>
+                        <lighting description="mass of ATA-33">
+                            <value>267.8019939</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </lighting>
+                        <fire_protection description="mass of ATA-26">
+                            <value>94.80332712</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </fire_protection>
+                        <oxygen_system description="mass of ATA-35">
+                            <value>114.784</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </oxygen_system>
+                        <flight_controls description="mass of ATA-27">
+                            <value>705.4785443</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </flight_controls>
+                        <instruments description="mass of ATA31">
+                            <value>87.77702173</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </instruments>
+                        <automatic_flight_system description="mass of ATA22">
+                            <value>142.6376603</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </automatic_flight_system>
+                        <navigation description="mass of ATA34">
+                            <value>581.5227689</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </navigation>
+                        <communication description="mass of ATA23">
+                            <value>285.2753206</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </communication>
+                        <bleed_air_system description="mass of ATA-36">
+                            <value>173.8881395</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </bleed_air_system>
+                        <hydraulic_generation description="mass of ATA-29">
+                            <value>180.7610158</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </hydraulic_generation>
+                        <hydraulic_distribution description="mass of ATA-29">
+                            <value>636.2256675</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </hydraulic_distribution>
+                        <electrical_generation description="mass of ATA-24">
+                            <value>746.0045998</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </electrical_generation>
+                        <electrical_distribution description="mass of ATA-24">
+                            <value>505.6840785</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </electrical_distribution>
+                        <auxiliary_power_unit description="mass of ATA-49">
+                            <value>217.7706588</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </auxiliary_power_unit>
+                        <air_conditioning description="mass of ATA-21">
+                            <value>762.7725196</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </air_conditioning>
+                    </mass_properties>
+                </geometry>
+                <maximium_power_demand description="maximum power (hydraulic + electric) demand">
+                    <value>365853.0145</value>
+                    <unit>W</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </maximium_power_demand>
+                <maximium_bleed_air_demand description="maximum bleed air demand">
+                    <value>2.370003007</value>
+                    <unit>kg/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </maximium_bleed_air_demand>
+                <average_power_demand description="average power (hydraulic + electric) demand">
+                    <value>117495.4149</value>
+                    <unit>W</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </average_power_demand>
+                <average_bleed_air_demand description="average bleed air demand">
+                    <value>1.024591634</value>
+                    <unit>kg/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </average_bleed_air_demand>
+            </specific>
+        </systems>
+        <fuselage description="Geometric description of the aircraft fuselage." tool_level="1">
+            <position description="Position of the fuselages with regard to the global reference point.">
+                <x description="Distance in x direction with regard to the global reference point. (fuselage nose point)">
+                    <value>-0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-100</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </x>
+                <y description="Distance in y direction with regard to the global reference point. (fuselage nose point)">
+                    <value>-0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-25</lower_boundary>
+                    <upper_boundary>25</upper_boundary>
+                </y>
+                <z description="Distance in z direction with regard to the global reference point. (fuselage nose point)">
+                    <value>-0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-5</lower_boundary>
+                    <upper_boundary>5</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of all fuselages.">
+                <mass description="Mass of all fuselages.">
+                    <value>17002.42932</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of all fuselages with regard to the total center of gravity.">
+                    <j_xx description="Inertia of the of all fuselages in x.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Inertia of the of all fuselages in y.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Inertia of the of all fuselages in z.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Inertia of all fuselages in xy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Inertia of all fuselages in xz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Inertia of all fuselages in yx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Inertia of all fuselages in yz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Inertia of all fuselages in zx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Inertia of all fuselages in zy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of all fuselages.">
+                    <x description="Center of gravity in x-direction with regard to the global reference point. (of all fuselages)">
+                        <value>16.8143301</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>50</upper_boundary>
+                    </x>
+                    <y description="Center of gravity in y-direction with regard to the global reference point. (of all fuselages)">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-5</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </y>
+                    <z description="Center of gravity in z-direction with regard to the global reference point. (of all fuselages)">
+                        <value>-0.2413</value>
+                        <unit>m</unit>
+                        <lower_boundary>-5</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific description="Fuselage design specific output parameter.">
+                <geometry description="Geometry description of the entire fuselage design.">
+                    <fuselage ID="0" description="Geometrical description of one entire fuselage.">
+                        <name description="Name of the fuselage.">
+                            <value>fuselage_0</value>
+                        </name>
+                        <position description="Position of one entire fuselage with regard to the fuselage global position.">
+                            <x description="Distance in x direction with regard to the fuselage gear global position.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the fuselage gear global position.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-25</lower_boundary>
+                                <upper_boundary>25</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the fuselage gear global position.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </position>
+                        <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                            <x description="X component of the unit vector.">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </x>
+                            <y description="Y component of the unit vector.">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </y>
+                            <z description="Z component of the unit vector.">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </z>
+                        </direction>
+                        <mass_properties description="Mass properties of one entire fuselage.">
+                            <mass description="Mass of one entire fuselage.">
+                                <value>17002.429319719</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>100000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire fuselage with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire fuselage in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire fuselage in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire fuselage in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire fuselage in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire fuselage in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire fuselage in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire fuselage in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire fuselage in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire fuselage in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire fuselage.">
+                                <x description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-25</lower_boundary>
+                                    <upper_boundary>25</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <sections description="Geometrical description of the fuselage sections of one entire fuselage.">
+                            <section ID="0" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_0</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.957580772</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.068075648</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.236859405</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.267845269</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>0.496500597</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="1" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_1</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.924669034</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.192850112</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.410780143</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.467251904</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>0.836740921</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="2" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_2</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.88671607</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.325974005</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.51432337</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.617142191</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.09949371</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="3" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_3</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.814819481</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.552671561</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.638938798</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.811819183</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.332869486</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="4" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_4</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.746964181</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.779068819</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.756396515</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.976541153</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.597847703</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="5" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_5</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.624593025</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>1.123655542</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.945319536</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.211739628</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.950706682</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="6" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_6</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.499674101</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>1.438280013</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.097107435</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.430154001</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>2.243644807</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="7" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_7</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.21769763</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>2.128158942</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.34967515</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.867790838</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>2.796234326</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="8" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_8</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.174885536</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>2.619107088</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.558414858</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.972433715</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.095828445</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="9" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_9</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.083279283</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>3.445878719</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.734079899</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.114075921</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.508608277</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="10" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_10</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.041639641</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>4.194982413</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.833938046</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.167619711</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.762303773</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="11" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_11</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>5.168818078</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.877197398</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.219703367</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.908262138</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="12" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_12</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>6.2175644</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915417119</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227583628</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="13" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_13</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>6.237748405</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915417119</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227583628</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="14" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_14</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>27.5216784</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915413925</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227579912</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="15" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_15</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>27.42759412</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915413925</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227579912</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="16" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_16</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>31.85324279</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.699062858</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.736999316</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.3288491</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="17" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_17</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>32.70160959</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.657090968</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.517589228</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.095828445</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="18" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_18</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>34.3983432</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.575335554</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.93980933</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>2.46334671</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="19" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_19</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0.92429206</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>37.35925828</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.528165979</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.614244216</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>0.559150813</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                        </sections>
+                        <number_of_required_cabin_crew description="Number of minimum required flight attendants.">
+                            <value>4</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </number_of_required_cabin_crew>
+                        <number_of_required_flight_crew description="Number of minimum required flight crew members.">
+                            <value>2</value>
+                            <unit>1</unit>
+                            <lower_boundary>1</lower_boundary>
+                            <upper_boundary>4</upper_boundary>
+                        </number_of_required_flight_crew>
+                        <mass_breakdown description="Mass breakdown of fuselage design module in accordance to CPACS.">
+                            <fuselage_structure description="Mass breakdown of the fuselage structure block.">
+                                <component_mass ID="0" description="Mass of a single component of the fuselage structure block.">
+                                    <name description="Name of the fuselage structure component.">
+                                        <value>door_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage structure component.">
+                                        <value>360.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="1" description="Mass of a single component of the fuselage structure block.">
+                                    <name description="Name of the fuselage structure component.">
+                                        <value>fuselage_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage structure component.">
+                                        <value>9187.161207458</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                            </fuselage_structure>
+                            <fuselage_furnishing description="Mass breakdown of the fuselage furnishing block.">
+                                <component_mass ID="0" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>lavatory_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>290.01</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="1" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>flight_attendant_seat_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>48.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="2" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>floor_covering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>159.641751426</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="3" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>wall_covering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>289.30950138</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="4" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>ceiling_covering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>106.98516576</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="5" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>linings_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>396.29466714</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="6" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>acoustic_and_thermal_insolation_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>619.575445338</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="7" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>overhead_bin_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>351.213928</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="8" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>passenger_safety_unit_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>90.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="9" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>lightning_panel_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>72.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="10" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>oxygen_system_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>201.51999999999998</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="11" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>cargo_linings_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>431.346961788</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="12" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>cargo_loadings_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>672.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="13" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>miscellaneous_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>324.160275369</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                            </fuselage_furnishing>
+                            <fuselage_operator_items description="Mass breakdown of the fuselage  operator items block.">
+                                <component_mass ID="0" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>total_emergency_equipment_masses</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>840.4850832</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="1" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>flight_attendant_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>280.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="2" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>flight_crew_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>170.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="3" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>in_flight_entertainment</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>90.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="4" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>total_fixed_galley_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>315.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="5" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>total_seat_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>1242.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="6" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>catering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>952.02</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                            </fuselage_operator_items>
+                        </mass_breakdown>
+                        <fuselage_accommodation description="Description of the accommodation of current fuselage.">
+                            <position description="Position of the payload tubes with regard to the fuselage position.">
+                                <x description="Distance in x direction with regard to the fuselage position.">
+                                    <value>3.75</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Distance in y direction with regard to the fuselage position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-0</lower_boundary>
+                                    <upper_boundary>0</upper_boundary>
+                                </y>
+                                <z description="Distance in z direction with regard to the fuselage position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <mass_properties description="Mass properties of the payload tubes of one entire fuselage.">
+                                <mass description="Mass of the payload tubes of one entire fuselage.">
+                                    <value>7455.268112261</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                                <center_of_gravity description="Center of gravity of all payload tubes.">
+                                    <x description="Center of gravity in x-direction with regard to the center of gravity of the fuselage.">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>50</upper_boundary>
+                                    </x>
+                                    <y description="Center of gravity in y-direction with regard to the center of gravity of the fuselage.">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-5</lower_boundary>
+                                        <upper_boundary>5</upper_boundary>
+                                    </y>
+                                    <z description="Center of gravity in z-direction with regard to the center of gravity of the fuselage.">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-5</lower_boundary>
+                                        <upper_boundary>5</upper_boundary>
+                                    </z>
+                                </center_of_gravity>
+                            </mass_properties>
+                            <payload_tube ID="0" description="Geometrical description of one payload tube of the fuselage.">
+                                <name description="Name of the payload tube.">
+                                    <value>center_payload_tube</value>
+                                </name>
+                                <payload_tube_reference_points description="Payload tube center reference points in x, y and z-direction referred to fuselage nose point.">
+                                    <front_reference_points description="Reference points in the front of payload tube.">
+                                        <x description="Payload tube reference point in x-direction.">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <y description="Payload tube reference point in y-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </y>
+                                        <z description="Payload tube reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                        <upper_z description="Upper payload tube reference point in z-direction.">
+                                            <value>1.778</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </upper_z>
+                                        <lower_z description="Lower payload tube reference point in z-direction.">
+                                            <value>-2.090166</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>0</upper_boundary>
+                                        </lower_z>
+                                    </front_reference_points>
+                                    <aft_reference_points description="Reference points in the aft of payload tube.">
+                                        <x description="Payload tube reference point in x-direction.">
+                                            <value>27.016456</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <y description="Payload tube reference point in y-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </y>
+                                        <z description="Payload tube reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                        <upper_z description="Upper payload tube reference point in z-direction.">
+                                            <value>1.778</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </upper_z>
+                                        <lower_z description="Lower payload tube reference point in z-direction.">
+                                            <value>-2.090166</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>0</upper_boundary>
+                                        </lower_z>
+                                    </aft_reference_points>
+                                </payload_tube_reference_points>
+                                <payload_tube_wall_reference_points description="Payload tube wall reference points in x, y and z-direction referred to fuselage nose point.">
+                                    <front_reference_points description="Reference points in the front of payload tube.">
+                                        <x description="Wall reference point in x-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <left_y description="Left wall reference point in y-direction.">
+                                            <value>-1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </left_y>
+                                        <right_y description="Right wall reference point in y-direction.">
+                                            <value>1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </right_y>
+                                        <z description="Wall reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                    </front_reference_points>
+                                    <aft_reference_points description="Reference points in the aft of payload tube.">
+                                        <x description="Wall reference point in x-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <left_y description="Left wall reference point in y-direction.">
+                                            <value>-1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </left_y>
+                                        <right_y description="Right wall reference point in y-direction.">
+                                            <value>1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </right_y>
+                                        <z description="Wall reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                    </aft_reference_points>
+                                </payload_tube_wall_reference_points>
+                                <payload_tube_structural_wall_thickness description="Structural wall thickness of the payload tube.">
+                                    <value>0.137414</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </payload_tube_structural_wall_thickness>
+                                <payload_tube_water_volume description="Total water volume of one entire payload tube.">
+                                    <value>188.945335573</value>
+                                    <unit>m^3</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1000</upper_boundary>
+                                </payload_tube_water_volume>
+                                <payload_decks description="Geometrical description of the payload decks.">
+                                    <payload_deck ID="0" description="Geometrical description of the payload decks in one payload tube.">
+                                        <name description="Name of the payload deck.">
+                                            <value>passenger_deck_1</value>
+                                        </name>
+                                        <position description="Position of the payload deck with regard to the payload tube reference point.">
+                                            <x description="Distance in x direction with regard to the payload tube reference point.">
+                                                <value>0.0</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-100</lower_boundary>
+                                                <upper_boundary>100</upper_boundary>
+                                            </x>
+                                            <y description="Distance in y direction with regard to the payload tube reference point.">
+                                                <value>0.0</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-0</lower_boundary>
+                                                <upper_boundary>0</upper_boundary>
+                                            </y>
+                                            <z description="Distance in z direction with regard to the payload tube reference point.">
+                                                <value>-0.4826</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-5</lower_boundary>
+                                                <upper_boundary>5</upper_boundary>
+                                            </z>
+                                        </position>
+                                        <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
+                                            <value>0.206248</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1</upper_boundary>
+                                        </payload_deck_structural_floor_thickness>
+                                        <payload_deck_water_volume description="Total water volume of the payload deck.">
+                                            <value>125.963557</value>
+                                            <unit>m^3</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1000</upper_boundary>
+                                        </payload_deck_water_volume>
+                                        <payload_deck_length description="Total length of the payload deck.">
+                                            <value>27.016456</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </payload_deck_length>
+                                        <payload_deck_required_galley_power description="Required galley power of the payload deck.">
+                                            <value>9000</value>
+                                            <unit>W</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100000</upper_boundary>
+                                        </payload_deck_required_galley_power>
+                                    </payload_deck>
+                                    <payload_deck ID="1" description="Geometrical description of the payload decks in one payload tube.">
+                                        <name description="Name of the payload deck.">
+                                            <value>cargo_deck</value>
+                                        </name>
+                                        <position description="Position of the payload deck with regard to the payload tube reference point.">
+                                            <x description="Distance in x direction with regard to the payload tube reference point.">
+                                                <value>3.75</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-100</lower_boundary>
+                                                <upper_boundary>100</upper_boundary>
+                                            </x>
+                                            <y description="Distance in y direction with regard to the payload tube reference point.">
+                                                <value>0.0</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-0</lower_boundary>
+                                                <upper_boundary>0</upper_boundary>
+                                            </y>
+                                            <z description="Distance in z direction with regard to the payload tube reference point.">
+                                                <value>-1.831848</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-5</lower_boundary>
+                                                <upper_boundary>5</upper_boundary>
+                                            </z>
+                                        </position>
+                                        <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
+                                            <value>0.206248</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1</upper_boundary>
+                                        </payload_deck_structural_floor_thickness>
+                                        <payload_deck_water_volume description="Total water volume of the payload deck.">
+                                            <value>62.98177852433333</value>
+                                            <unit>m^3</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1000</upper_boundary>
+                                        </payload_deck_water_volume>
+                                        <payload_deck_length description="Total length of the payload deck.">
+                                            <value>13.508228</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </payload_deck_length>
+                                        <payload_deck_required_galley_power description="Required galley power of the payload deck.">
+                                            <value>0</value>
+                                            <unit>W</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100000</upper_boundary>
+                                        </payload_deck_required_galley_power>
+                                    </payload_deck>
+                                </payload_decks>
+                            </payload_tube>
+                        </fuselage_accommodation>
+                    </fuselage>
+                </geometry>
+            </specific>
+        </fuselage>
+        <tank description="Description of aircraft tanks." tool_level="2">
+            <position description="Tank reference point, position of the tanks with regard to the global reference point.">
+                <x description="Distance between the foremost tank end and the global reference point in x-direction.">
+                    <value>11.39593946</value>
+                    <unit>m</unit>
+                    <lower_boundary>-80</lower_boundary>
+                    <upper_boundary>80</upper_boundary>
+                </x>
+                <y description="Distance between the foremost tank end and the global reference point in y-direction.">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-40</lower_boundary>
+                    <upper_boundary>40</upper_boundary>
+                </y>
+                <z description="Distance between the foremost middle tank end and the global reference point in z-direction.">
+                    <value>-1.030571436</value>
+                    <unit>m</unit>
+                    <lower_boundary>-5</lower_boundary>
+                    <upper_boundary>5</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of all tanks.">
+                <mass description="Total tank mass.">
+                    <value>0.0</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of all tanks with regard to the total center of gravity.">
+                    <j_xx description="Inertia of all tanks in x.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Inertia of all tanks in y.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Inertia of all tanks in z.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Inertia of all tanks in xy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Inertia of all tanks in xz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Inertia of all tanks in yx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Inertia of all tanks in yz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Inertia of all tanks in zx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Inertia of all tanks in zy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of all tanks.">
+                    <x description="Center of gravity in x-direction with regard to the global reference point.">
+                        <value>0.0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-80</lower_boundary>
+                        <upper_boundary>80</upper_boundary>
+                    </x>
+                    <y description="Center of gravity in y-direction with regard to the global reference point.">
+                        <value>0.0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-40</lower_boundary>
+                        <upper_boundary>40</upper_boundary>
+                    </y>
+                    <z description="Center of gravity in z-direction with regard to the global reference point.">
+                        <value>0.0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-5</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific description="Tank design specific output parameter.">
+                <additional_fuselage_length description="Additional fuselage length (if smaller than 0: shrink fuselage, if greater than 0: stretch fuselage).">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </additional_fuselage_length>
+                <tank ID="0" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_0</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_inner_left</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>1.286074111</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>-1.983993414</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>1.168691393</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>-2.642463092</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.386238922</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>1.761785342e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>true</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.8681000247344418</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>2.5721482215999996</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>1.653528351</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.234107584</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>-3.347894434</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.5670835447557853</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.8331119023999998</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="1" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_1</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_outer_left</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>2.939602462</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>-5.331887848</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.234107584</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>0.843411494</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>-6.9686868</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.258517685</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>1.789109824e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>true</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.5670835447557853</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.8331119023999998</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>4.414633554</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.859474552</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>-9.188112152</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.21429889577770245</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>0.801935759545338</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="2" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_2</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_inner_right</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>1.286074111</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>1.983993414</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>1.168691393</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>2.642463092</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.386238922</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>1.761785342e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>true</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.8681000247344418</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>2.5721482215999996</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>1.653528351</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.234107584</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>3.347894434</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.5670835447557853</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.8331119023999998</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="3" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_3</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_outer_right</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>2.939602462</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>5.331887848</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.234107584</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>0.843411494</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>6.9686868</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.258517685</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>1.789109824e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>true</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.5670835447557853</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.8331119023999998</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>4.414633554</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.859474552</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>9.188112152</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.21429889577770245</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>0.801935759545338</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="4" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_4</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_center</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>1.286074111</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>1.286074111</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>0</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>false</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.98207674</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.8681000247344418</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>2.5721482215999996</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>-0.98207674</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.8681000247344418</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>2.5721482215999996</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+            </specific>
+        </tank>
+        <landing_gear description="Geometric description of the aircraft undercarriage." tool_level="3">
+            <position description="Position of the total undercarriage arrangement with regard to the global reference point.">
+                <x description="Distance in x direction with regard to the global reference point. (total undercarriage arrangement)">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-100</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </x>
+                <y description="Distance in y direction with regard to the global reference point. (total undercarriage arrangement)">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-25</lower_boundary>
+                    <upper_boundary>25</upper_boundary>
+                </y>
+                <z description="Distance in z direction with regard to the global reference point. (total undercarriage arrangement)">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-10</lower_boundary>
+                    <upper_boundary>10</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of the total undercarriage arrangement.">
+                <mass description="Mass of the total undercarriage arrangement.">
+                    <value>3093.1066</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of the total undercarriage arrangement with regard to the total center of gravity.">
+                    <j_xx description="Inertia of the total undercarriage arrangement in x.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Inertia of the total undercarriage arrangement in y.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Inertia of the total undercarriage arrangement in z.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Inertia of the total undercarriage arrangement in xy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Inertia of the total undercarriage arrangement in xz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Inertia of the total undercarriage arrangement in yx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Inertia of the total undercarriage arrangement in yz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Inertia of the total undercarriage arrangement in zx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Inertia of the total undercarriage arrangement in zy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of the total undercarriage arrangement.">
+                    <x description="Center of gravity in x-direction with regard to the global reference point. (total undercarriage arrangement)">
+                        <value>14.7445</value>
+                        <unit>m</unit>
+                        <lower_boundary>-100</lower_boundary>
+                        <upper_boundary>100</upper_boundary>
+                    </x>
+                    <y description="Center of gravity in y-direction with regard to the global reference point. (total undercarriage arrangement)">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-50</lower_boundary>
+                        <upper_boundary>50</upper_boundary>
+                    </y>
+                    <z description="Center of gravity in z-direction with regard to the global reference point. (total undercarriage arrangement)">
+                        <value>-1.6458</value>
+                        <unit>m</unit>
+                        <lower_boundary>-10</lower_boundary>
+                        <upper_boundary>10</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <aircraft_classification_number description="Aircraft classification number for the total undercarriage arrangement. (CBR = [3, 6, 10, 15])">
+                <value>[55.3, 49.5, 45.0, 43.1]</value>
+            </aircraft_classification_number>
+            <specific description="Landing gear specific output parameter.">
+                <geometry description="Geometry description of the entire landing gear.">
+                    <landing_gear_assembly ID="0" description="Geometrical description of one entire landing gear leg.">
+                        <name description="Name of the landing gear leg.">
+                            <value>nose_gear_assembly</value>
+                        </name>
+                        <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+                            <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>5.05</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-50</lower_boundary>
+                                <upper_boundary>50</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-1.6572</value>
+                                <unit>m</unit>
+                                <lower_boundary>-10</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of one entire landing gear leg.">
+                            <mass description="Mass of one entire landing gear leg.">
+                                <value>461.4583</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire landing gear leg in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire landing gear leg in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire landing gear leg in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire landing gear leg in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire landing gear leg in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire landing gear leg in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire landing gear leg in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire landing gear leg in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire landing gear leg in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+                                <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>-10.7433</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-50</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.0114</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-10</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+                            <strut_diameter description="Diameter of the landing gear strut">
+                                <value>0.3556</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.0</upper_boundary>
+                            </strut_diameter>
+                            <strut_length description="Length of the landing gear strut">
+                                <value>2.0976</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </strut_length>
+                            <tire_description ID="0" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00453-C</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>-0.5334</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.0976</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.0109</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.3556</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                            <tire_description ID="1" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00453-C</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>0.5334</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.0976</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.0109</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.3556</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                        </assembly_components>
+                    </landing_gear_assembly>
+                    <landing_gear_assembly ID="1" description="Geometrical description of one entire landing gear leg.">
+                        <name description="Name of the landing gear leg.">
+                            <value>right_main_gear_outer_strut</value>
+                        </name>
+                        <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+                            <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>16.6283</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>4.4965</value>
+                                <unit>m</unit>
+                                <lower_boundary>-50</lower_boundary>
+                                <upper_boundary>50</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-0.8554</value>
+                                <unit>m</unit>
+                                <lower_boundary>-10</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of one entire landing gear leg.">
+                            <mass description="Mass of one entire landing gear leg.">
+                                <value>1315.8242</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire landing gear leg in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire landing gear leg in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire landing gear leg in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire landing gear leg in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire landing gear leg in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire landing gear leg in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire landing gear leg in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire landing gear leg in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire landing gear leg in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+                                <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.4341</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+                                    <value>4.4965</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-50</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.2159</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-10</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+                            <strut_diameter description="Diameter of the landing gear strut">
+                                <value>0.2322</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.0</upper_boundary>
+                            </strut_diameter>
+                            <strut_length description="Length of the landing gear strut">
+                                <value>2.8994</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </strut_length>
+                            <tire_description ID="0" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>-0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.8994</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                            <tire_description ID="1" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.8994</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                        </assembly_components>
+                    </landing_gear_assembly>
+                    <landing_gear_assembly ID="2" description="Geometrical description of one entire landing gear leg.">
+                        <name description="Name of the landing gear leg.">
+                            <value>left_main_gear_outer_strut</value>
+                        </name>
+                        <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+                            <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>16.6283</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-4.4965</value>
+                                <unit>m</unit>
+                                <lower_boundary>-50</lower_boundary>
+                                <upper_boundary>50</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-0.8554</value>
+                                <unit>m</unit>
+                                <lower_boundary>-10</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of one entire landing gear leg.">
+                            <mass description="Mass of one entire landing gear leg.">
+                                <value>1315.8242</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire landing gear leg in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire landing gear leg in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire landing gear leg in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire landing gear leg in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire landing gear leg in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire landing gear leg in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire landing gear leg in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire landing gear leg in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire landing gear leg in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+                                <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.4341</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+                                    <value>4.4965</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-50</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.2159</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-10</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+                            <strut_diameter description="Diameter of the landing gear strut">
+                                <value>0.2322</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.0</upper_boundary>
+                            </strut_diameter>
+                            <strut_length description="Length of the landing gear strut">
+                                <value>2.8994</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </strut_length>
+                            <tire_description ID="0" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>-0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.8994</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                            <tire_description ID="1" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-2.8994</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                        </assembly_components>
+                    </landing_gear_assembly>
+                </geometry>
+            </specific>
+        </landing_gear>
+    </component_design>
+    <sizing_point>
+        <thrust_to_weight description="Total thrust (kN) divided by maximum aircraft weight (kN)">
+            <value>0.3264602941</value>
+            <unit>1</unit>
+            <lower_boundary>-1.797693135e+308</lower_boundary>
+            <upper_boundary>1.797693135e+308</upper_boundary>
+        </thrust_to_weight>
+        <wing_loading description="Maximum takeoff mass (MTOM) divided by wing area (Sref)">
+            <value>594</value>
+            <unit>kg/m^2</unit>
+            <lower_boundary>-inf</lower_boundary>
+            <upper_boundary>inf</upper_boundary>
+        </wing_loading>
+    </sizing_point>
+    <assessment description="Assessment data">
+        <performance description="Assessment of performance values">
+            <takeoff description="Takeoff assessment">
+                <takeoff_distance_normal_safety description="Takeoff distance at Sea Level for MTOM and (ISA + deltaISA)-Conditions(calculated by mission_analysis using missionDesign.xml settings) with all engines operating (AEO)">
+                    <value>1002.479852</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </takeoff_distance_normal_safety>
+                <lift_off_speed_velocity description="Lift off velocity">
+                    <value>67.14382991</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>400</upper_boundary>
+                </lift_off_speed_velocity>
+                <takeoff_safety_speed description="Take off safety speed (V2)">
+                    <value>67.14382991</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>200</upper_boundary>
+                </takeoff_safety_speed>
+                <final_takeoff_speed description="Final take off speed">
+                    <value>98.21570864</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>200</upper_boundary>
+                </final_takeoff_speed>
+                <time_to_screen_height description="Time to screen height">
+                    <value>30.33908686</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>3600</upper_boundary>
+                </time_to_screen_height>
+                <climb_or_descend_segment_climb_gradient description="Climb or descend in second segment">
+                    <value>3.891003875</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </climb_or_descend_segment_climb_gradient>
+                <final_segment_climb_gradient description="Climb gradient in final segment">
+                    <value>3.891003875</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </final_segment_climb_gradient>
+            </takeoff>
+            <altitude description="Assessment of altitude related values">
+                <maximum_operating_altitude description="Maximum operating altitude (100 ft/min rate of climb)">
+                    <value>12538.07112</value>
+                    <unit>m</unit>
+                    <lower_boundary>4500</lower_boundary>
+                    <upper_boundary>20000</upper_boundary>
+                </maximum_operating_altitude>
+                <maximum_ceiling_altitude description="Maximum operating altitude (50 ft/min rate of climb)">
+                    <value>12665.55421</value>
+                    <unit>m</unit>
+                    <lower_boundary>4500</lower_boundary>
+                    <upper_boundary>20000</upper_boundary>
+                </maximum_ceiling_altitude>
+                <maximum_altitude_one_engine_inoperative description="Maximum operating altitude with one engine inoperative (100 ft/min rate of climb)">
+                    <value>6698.267578</value>
+                    <unit>m</unit>
+                    <lower_boundary>1500</lower_boundary>
+                    <upper_boundary>12000</upper_boundary>
+                </maximum_altitude_one_engine_inoperative>
+            </altitude>
+            <climb description="Assessment of the climb segment">
+                <design_time_to_climb description="Time needed to climb from 1500ft to ICA (ISA + deltaISA)">
+                    <value>1043.433728</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>7200</upper_boundary>
+                </design_time_to_climb>
+                <time_to_1500ft_ISA description="Time needed to climb from break release to 1500ft (ISA + deltaISA)">
+                    <value>71.71860527</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>7200</upper_boundary>
+                </time_to_1500ft_ISA>
+                <time_to_ICA_ISA description="Time needed to climb from break release to ICA (ISA + deltaISA)">
+                    <value>1115.152333</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>7200</upper_boundary>
+                </time_to_ICA_ISA>
+                <range_to_ICA_ISA description="Range needed to climb from break release to ICA (ISA + deltaISA)">
+                    <value>206140.7922</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>500000</upper_boundary>
+                </range_to_ICA_ISA>
+                <fuel_to_ICA_ISA description="Fuel mass needed to climb from break release to ICA (ISA + deltaISA)">
+                    <value>1391.253999</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>10000</upper_boundary>
+                </fuel_to_ICA_ISA>
+            </climb>
+            <speed>
+                <maximum_operating_mach_number description="Maximum operating mach number">
+                    <value>0.82</value>
+                    <unit>1</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1</upper_boundary>
+                </maximum_operating_mach_number>
+                <maximum_operating_velocity description="Maximum operating velocity">
+                    <value>180</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>400</upper_boundary>
+                </maximum_operating_velocity>
+                <dive_mach_number description="Maximum dive mach number">
+                    <value>0.902</value>
+                    <unit>1</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1</upper_boundary>
+                </dive_mach_number>
+                <dive_velocity description="Dive velocity">
+                    <value>198</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>400</upper_boundary>
+                </dive_velocity>
+                <one_g_stall_speed_velocity description="One g stall speed">
+                    <value>76.59880474</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>400</upper_boundary>
+                </one_g_stall_speed_velocity>
+            </speed>
+            <landing>
+                <needed_runway_length description="Needed runway length">
+                    <value>1552.150628</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>100000</upper_boundary>
+                </needed_runway_length>
+                <approach_speed description="Approach speed">
+                    <value>62.17437344</value>
+                    <unit>m/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1000</upper_boundary>
+                </approach_speed>
+            </landing>
+            <range>
+                <range_max_payload_at_maximum_takeoff_mass description="Range at max payload at maximum take off mass">
+                    <value>4538395.775</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </range_max_payload_at_maximum_takeoff_mass>
+                <range_max_fuel_at_maximum_takeoff_mass description="Range at max fuel at maximum take off mass">
+                    <value>5522113.489</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </range_max_fuel_at_maximum_takeoff_mass>
+                <payload_maximum_fuel_at_maximum_takeoff_mass description="Payload at maximum fuel at maximum takeoff mass">
+                    <value>17768.3076</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </payload_maximum_fuel_at_maximum_takeoff_mass>
+                <range_maximum_fuel_empty description="Range at maximum fuel empty">
+                    <value>6821947.039</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </range_maximum_fuel_empty>
+            </range>
+        </performance>
+        <cost_estimation description="Cost estimation results" tool_level="2">
+            <operating_cost description="Operating cost estimation results" tool_level="0">
+                <direct_operating_cost description="Direct operating cost (sum of route independent and route dependent cost)" tool_level="0">
+                    <flights_per_year_design_mission description="Flights per year (design mission)">
+                        <value>808.237248168613</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>100000</upper_boundary>
+                    </flights_per_year_design_mission>
+                    <route_independent_cost_annual description="Route independent (fixed) cost per year">
+                        <value>11379945.701676166</value>
+                        <unit>USD/a</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </route_independent_cost_annual>
+                    <route_dependent_cost_annual description="Route dependent (variable) cost per year">
+                        <value>20109814.306327358</value>
+                        <unit>USD/a</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </route_dependent_cost_annual>
+                    <direct_operating_cost_annual description="Direct operating cost (DOC) per year">
+                        <value>31489760.008003525</value>
+                        <unit>USD/a</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </direct_operating_cost_annual>
+                    <flights_per_year_study_mission description="Flights per year (study mission)">
+                        <value>2000</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>100000</upper_boundary>
+                    </flights_per_year_study_mission>
+                </direct_operating_cost>
+            </operating_cost>
+        </cost_estimation>
+        <ecological_assessment description="Ecological assessment data" />
+        <operating_cost_estimation_tu_berlin description="Operating costs (sum of direct and indirect operating costs)" tool_level="2">
+            <direct_operating_costs description="Direct operating costs (sum of route independent and route dependent costs)">
+                <direct_operating_costs_annual description="Direct operating costs (DOC) per year">
+                    <value>30</value>
+                    <unit>EUR/y</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </direct_operating_costs_annual>
+            </direct_operating_costs>
+            <indirect_operating_costs description="Indirect operating costs (IOC)">
+                <indirect_operating_costs_annual description="Indirect operating costs (IOC) per year">
+                    <value>40</value>
+                    <unit>EUR/y</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </indirect_operating_costs_annual>
+            </indirect_operating_costs>
+        </operating_cost_estimation_tu_berlin>
+    </assessment>
+    <requirement_compliance description="Compliance of given requirements">
+        <top_level_aircraft_requirements description="Compliance of top level aircraft requirements">
+            <initial_cruise_altitude description="Compliance check of the initial cruise altitude.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </initial_cruise_altitude>
+            <initial_cruise_mach_number description="Compliance check of the initial cruise mach number.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </initial_cruise_mach_number>
+            <maximum_operating_altitude description="Compliance check of the maximum operating altitude.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </maximum_operating_altitude>
+            <maximum_altitude_one_engine_inoperative description="Compliance check of the maximum altitude one engine inoperative.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </maximum_altitude_one_engine_inoperative>
+            <design_time_to_climb description="Compliance check of the design time to climb.">
+                <maintainable description="Value shows if the requirement can be achieved by the aircraft.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </design_time_to_climb>
+            <design_takeoff_distance description="Compliance check of the design takeoff distance.">
+                <maintainable description="Switch indicating if design takeoff distance can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </design_takeoff_distance>
+            <design_landing_field_length description="Compliance check of the design landing field length.">
+                <maintainable description="Switch indicating if landing field length can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </design_landing_field_length>
+            <design_approach_speed description="Compliance check of the design approach speed.">
+                <maintainable description="Switch indicating if approach speed can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </design_approach_speed>
+            <span_limit>
+                <maintainable description="Switch indicating if the span limit according to ICAO aerodrome ref code is maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </span_limit>
+        </top_level_aircraft_requirements>
+        <certification>
+            <climb_gradient_of_second_takeoff_segment>
+                <maintainable description="Switch indicating if climb gradient of second takeoff segment can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </climb_gradient_of_second_takeoff_segment>
+            <climb_gradient_of_final_takeoff_segment>
+                <maintainable description="Switch indicating if climb gradient of final takeoff segment can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </climb_gradient_of_final_takeoff_segment>
+            <climb_gradient_approach_one_engine_inoperative>
+                <maintainable description="Switch indicating if climb gradient approach one engine inoperative can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </climb_gradient_approach_one_engine_inoperative>
+            <climb_gradient_all_engines_operative>
+                <maintainable description="Switch indicating if climb gradient with all engines operative can be maintained.">
+                    <value>true</value>
+                </maintainable>
+                <checked description="Indicates if the value has been checked against the requirement.">
+                    <value>true</value>
+                </checked>
+            </climb_gradient_all_engines_operative>
+        </certification>
+    </requirement_compliance>
+</aircraft_exchange_file>
\ No newline at end of file
diff --git a/mkdocs.yml b/mkdocs.yml
index 48527a25131c2fdf0e30f4025f051948799f832b..853972602dfbf88aaa91abfc08b7e2e4f742fbad 100644
--- a/mkdocs.yml
+++ b/mkdocs.yml
@@ -193,6 +193,20 @@ plugins:
             OUTPUT_DIR: "docs/api/aircraft_geometry2"
           src-dirs: aircraft-design/libs/aircraftGeometry2/src/
           full-doc: true
+        airfoils:
+          doxyfile: Doxyfile
+          variables:
+            PROJECT_NAME: "airfoils"
+            OUTPUT_DIR: "docs/api/airfoils"
+          src-dirs: ../aircraft-design/libs/airfoils/src/
+          full-doc: true
+        aixml:
+          doxyfile: Doxyfile
+          variables:
+            PROJECT_NAME: "aixml"
+            OUTPUT_DIR: "docs/api/aixml"
+          src-dirs: ../aircraft-design/libs/aixml/src/
+          full-doc: true
         engine:
           variables:
             PROJECT_NAME: "engine"
@@ -263,11 +277,6 @@ nav:                                      # Customizes the main navigation struc
             - Getting Started: documentation/sizing/create_mission_xml/getting_started.md
             - Mission Steps: documentation/sizing/create_mission_xml/mission_steps.md
             - Airports: documentation/sizing/create_mission_xml/airports.md
-            - API Reference:
-              - create_mission_xml/classes.md
-              - create_mission_xml/namespaces.md
-              - create_mission_xml/files.md
-              - create_mission_xml/functions.md
           - Fuselage Design:
             - Introduction: documentation/sizing/fuselage_design/index.md
             - Getting Started: documentation/sizing/fuselage_design/getting_started.md
@@ -424,6 +433,24 @@ nav:                                      # Customizes the main navigation struc
             - aircraftGeometry2/namespaces.md
             - aircraftGeometry2/files.md
             - aircraftGeometry2/functions.md
+        - airfoils:
+          - Introduction: documentation/libraries/airfoils/index.md
+          - API Reference:
+            - airfoils/classes.md
+            - airfoils/namespaces.md
+            - airfoils/files.md
+            - airfoils/functions.md
+        - aixml:
+          - Introduction: documentation/libraries/aixml/index.md
+          - Endnode:
+            - Introduction: documentation/libraries/aixml/endnode/index.md
+            - Valid Units: documentation/libraries/aixml/endnode/valid_units.md
+            - Getting Started: documentation/libraries/aixml/endnode/getting-started.md
+          - API Reference:
+            - aixml/classes.md
+            - aixml/namespaces.md
+            - aixml/files.md
+            - aixml/functions.md
         - engine:
           - Overview:
             - documentation/libraries/engine/index.md