From d7eb7aff4fec2ca128da820da6bfe157fdc039ae Mon Sep 17 00:00:00 2001
From: Heinz-Ullrich Rings <ullrich.rings@ilr.rwth-aachen.de>
Date: Mon, 4 Nov 2024 10:25:14 +0100
Subject: [PATCH] changed settings page to parse and display csmr-2020 file,
also added backend point to get it
---
UnicadoGUI/Backend/main.py | 11 +-
UnicadoGUI/Backend/xml_configs/csmr-2020.xml | 9187 +++++++++++++++++
.../Frontend/src/routes/settings/+page.svelte | 263 +-
3 files changed, 9453 insertions(+), 8 deletions(-)
create mode 100644 UnicadoGUI/Backend/xml_configs/csmr-2020.xml
diff --git a/UnicadoGUI/Backend/main.py b/UnicadoGUI/Backend/main.py
index 79989766..773e5da2 100644
--- a/UnicadoGUI/Backend/main.py
+++ b/UnicadoGUI/Backend/main.py
@@ -15,6 +15,7 @@ app = FastAPI()
origins = [
"http://localhost",
"http://localhost:5173",
+ "http://localhost:5174",
]
app.add_middleware(
@@ -135,4 +136,12 @@ async def upload_project_list(file: UploadFile = File(...)):
@app.get("/projects/")
async def get_project_list():
file_path = UPLOAD_DIRECTORY + "projects.zip"
- return FileResponse(path=file_path, filename="projects.zip", media_type="application/zip")
\ No newline at end of file
+ return FileResponse(path=file_path, filename="projects.zip", media_type="application/zip")
+
+#TODO get file per project
+#endpoint to get the aircraft_exchange_file
+@app.get("/projects/aircraft_exchange_file/")
+async def get_aircraft_exchange_file():
+ with open("xml_configs/csmr-2020.xml", encoding='utf-8') as fd:
+ config = json.dumps(xmltodict.parse(fd.read()))
+ return config
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/csmr-2020.xml b/UnicadoGUI/Backend/xml_configs/csmr-2020.xml
new file mode 100644
index 00000000..9df1fb1b
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/csmr-2020.xml
@@ -0,0 +1,9187 @@
+<aircraft_exchange_file>
+ <requirements_and_specifications description="Requirements and specifications">
+ <general description="General aircraft information">
+ <type description="Aircraft type">
+ <value>CeRAS</value>
+ </type>
+ <model description="Model - Version">
+ <value>SMR-2020</value>
+ </model>
+ </general>
+ <mission_files description="Name of xml files which are located in the missionData 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">
+ <aerodynamic_technologies description="Integration of aerodynamic technologies on the aircraft: true / false">
+ <value>false</value>
+ </aerodynamic_technologies>
+ <configuration_type description="aircraft configuration: tube_and_wing / blended_wing_body">
+ <value>tube_and_wing</value>
+ </configuration_type>
+ <fuselage_definition description="Design description of the fuselage.">
+ <fuselage_type description="Fuselage type: single_aisle / wide_body">
+ <value>single_aisle</value>
+ </fuselage_type>
+ <fuselage_pressurization description="Switch to select a pressurized fuselage. (true: pressurized fuselage, false: non pressurized fuselage)">
+ <value>true</value>
+ </fuselage_pressurization>
+ <blended_wing_body_configuration description="Additional design description for blended wing body configurations.">
+ <number_of_payload_tubes description="Number of fuselage tubes for blendend wing body configurations. For tube and wing configuration is set to 1.">
+ <value>1</value>
+ <unit>1</unit>
+ <default>1</default>
+ <lower_boundary>1</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </number_of_payload_tubes>
+ <center_body_wing_sweep description="Sweep of the leading edge of the center body.">
+ <value>60</value>
+ <unit>degree</unit>
+ <default>60</default>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ <center_body_wing_sweep_tolerance Desc="Permissible deviation of the actual from the desired leading edge sweep of the center body.">
+ <value>5</value>
+ <unit>degree</unit>
+ <default>5</default>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </center_body_wing_sweep_tolerance>
+ </center_body_wing_sweep>
+ </blended_wing_body_configuration>
+ </fuselage_definition>
+ <wing_definition description="Definitions for wing design">
+ <mounting description="wing mounting for tube_and_wing configuration (ignored at blended_wing_body) - low / mid / high">
+ <value>low</value>
+ </mounting>
+ </wing_definition>
+ <empennage_definition description="Definitions for empennage design">
+ <empennage_type description="tube_and_wing configuration: conventional - blended_wing_body: vertical_tails">
+ <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: wing_mounted / fuselage_mounted.">
+ <value>wing_mounted</value>
+ </main_gear_mounting>
+ <undercarriage_retractability description="Switch to set retractability of landing gear: retractable / non_retractable.">
+ <value>retractable</value>
+ </undercarriage_retractability>
+ </undercarriage_definition>
+ <tank_definition description="Energy tanks information">
+ <tank ID="0" description="One 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: tailcone, rear, front, top, bottom, 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). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <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="single 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: tailcone, rear, front, top, bottom, 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). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <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="single 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: tailcone, rear, front, top, bottom, 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). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <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="single 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: tailcone, rear, front, top, bottom, 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). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <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="single 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: tailcone, rear, front, top, bottom, 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). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <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="maximum 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>
+ </configuration>
+ <transport_task>
+ <passenger_definition description="Define the masses of the passengers">
+ <total_number_passengers description="Design number of passengers">
+ <value>162</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 a the luggage for a single passenger">
+ <value>17</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. (true: multi passenger deck allowed, false: multi passenger deck denied)">
+ <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>0/0/0/0.1/0.9</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>500</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</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 / liquid_hydrogen / battery / saf">
+ <value>kerosene</value>
+ </type>
+ <density description="Energy carrier density.">
+ <value>783</value>
+ <unit>kg/m^3</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10000</upper_boundary>
+ </density>
+ <volumetric_density description="Volumetric energy density of energy carrier.">
+ <value>3.2325e+10</value>
+ <unit>J/m^3</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</upper_boundary>
+ </volumetric_density>
+ <gravimetric_density description="Gravimetric energy density of energy carrier.">
+ <value>43100000</value>
+ <unit>J/kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</upper_boundary>
+ </gravimetric_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 / electric / fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <type description="Type of main thrust generator. Selector: fan / prop">
+ <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 / electric / fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <type description="Type of main thrust generator. Selector: fan / prop">
+ <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">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <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">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <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">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <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">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <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">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <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">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <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">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <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>
+ <skinning description="Skinning Information">
+ <material description="Material of skinning">
+ <value>aluminium2024</value>
+ </material>
+ <thickness description="Thickness of skinning">
+ <value>0.003</value>
+ <unit>m</unit>
+ <lower_boundary>0.0001</lower_boundary>
+ <upper_boundary>0.1</upper_boundary>
+ </thickness>
+ </skinning>
+ <technology>
+ <variable_camber description="Switch if variable camber is used">
+ <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 structual payload mass which can be carried by the aircraft (e.g. for short trips)">
+ <value>30000</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 landiung mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)">
+ <value>2425</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>3CIIIB</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_one_engine_operating_altitude 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_one_engine_operating_altitude>
+ <climb_or_descend_segment_gradient description="climb / descend segment gradient">
+ <value>0.024</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </climb_or_descend_segment_gradient>
+ </flight_envelope>
+ <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>
+ <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 the specified mission">
+ <value>4537400</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>20000000</upper_boundary>
+ </range>
+ <contingency description="Reserved Fuel Percentage">
+ <value>0.06</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>0.08</upper_boundary>
+ </contingency>
+ <alt_dist description="Reserved fuel - alternate distance">
+ <value>370400</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>926000</upper_boundary>
+ </alt_dist>
+ <loiter_time description="Reserved fuel - loiter time in seconds">
+ <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 specified 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>
+ <breaking_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>
+ </breaking_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="2">
+ <maximum_takeoff_mass>
+ <mass_properties>
+ <mass description="mass">
+ <value>64586.71283</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>300000</upper_boundary>
+ </mass>
+ <inertia>
+ <j_xx description="inertia in x">
+ <value>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</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</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</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</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</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</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</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</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity>
+ <x description="x component">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </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>599569.7918648543</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>1693729.8225431978</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>2250064.0202634176</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>15.65578242991758</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>0.0016924404193550643</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>-0.7686391127807779</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <mass description="Mass">
+ <value>36354.8858137</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ </mass_properties>
+ </operating_mass_empty>
+ <design_mass description="">
+ <mass_properties description="design mass properties">
+ <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>15.822140859635715</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>0.0009526491672380705</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>-0.49323187357341247</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <mass description="Mass">
+ <value>64586.71283</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>1065172.977496338</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>3009016.235693439</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>3997378.4946150086</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>
+ </mass_properties>
+ </design_mass>
+ <most_forward_mass description="">
+ <mass_properties description="most forward mass properties">
+ <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>14.971565471999668</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>54132.712830000004</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>599569.7918648543</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>1693729.8225431978</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>2250064.0202634176</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>
+ </mass_properties>
+ </most_forward_mass>
+ <most_afterward_mass description="">
+ <mass_properties description="most afterward mass properties">
+ <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>16.190913398360987</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>55092.712830000004</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>599569.7918648543</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>1693729.8225431978</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>2250064.0202634176</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>
+ </mass_properties>
+ </most_afterward_mass>
+ <manufacturer_mass_empty description="MME">
+ <mass_properties description="manufacturer mass empty properties">
+ <mass description="Mass">
+ <value>33257.8766177</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>548493.488983179</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>1549443.938581515</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>2058384.9981354333</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>15.654878612191535</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>0.0018500372003712442</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>-0.8402133014801614</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </manufacturer_mass_empty>
+ <maximum_zero_fuel_mass description="MZFM">
+ <mass_properties description="maximum zero fuel mass properties">
+ <mass description="Mass">
+ <value>66354.8858137</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>1094333.9302566017</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>3091393.260043198</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>4106813.645439384</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>16.123871067575358</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>0.0009272637189805906</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>-0.5302215013355478</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_zero_fuel_mass>
+ <maximum_payload_mass description="">
+ <mass_properties description="maximum payload mass properties">
+ <mass description="Mass">
+ <value>30000.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <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>16.6911147</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_properties>
+ </maximum_payload_mass>
+ <maximum_landing_mass description="MLM">
+ <mass_properties description="maximum landing mass properties">
+ <mass description="Mass">
+ <value>55289.67959760656</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>911845.0229355189</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>2575878.7881554803</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>3421969.728965175</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>15.65578242991758</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>0.0016924404193550643</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>-0.7686391127807779</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_landing_mass>
+ <maximum_fuel_mass description="">
+ <mass_properties description="maximum fuel mass properties">
+ <mass description="Mass">
+ <value>53058.889254535265</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <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>15.409485429697211</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>0.0011596262013133772</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>-0.5266560904250428</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_fuel_mass>
+ </masses_cg_inertia>
+ <aerodynamics>
+ <lift_coefficients description="lift coefficients">
+ <C_LoptimumCruise description="optimum cruise CL">
+ <value>0.556</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </C_LoptimumCruise>
+ <C_LmaxLanding description="C_LmaxLanding">
+ <value>1.629</value>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </C_LmaxLanding>
+ <C_LmaxT-O description="C_LmaxTO">
+ <value>1.627</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>
+ <polar>
+ <polar_file description="Name of polar file">
+ <value>SMR-2020_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>32.9299991</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </b>
+ <MAC description="Mean aerodynamic chord">
+ <value>3.857492149</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </MAC>
+ <S_ref description="Wing reference area">
+ <value>105.2800817</value>
+ <unit>m^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </S_ref>
+ </reference_values>
+ <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>4538402.27</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000000</upper_boundary>
+ </range>
+ <mission_energy ID="0" description="Amount of energy loaded into tanks (including reserves) for specified energy carrier">
+ <consumed_energy description="Energy amount">
+ <value>5.510329405e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</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>
+ <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>4.494145685e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</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>
+ <taxi_energy ID="0" description="Amount of energy needed for taxi segment specified energy carrier">
+ <consumed_energy description="Energy amount">
+ <value>1.299219544e+10</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</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_energy>
+ <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
+ <value>20978.31905</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>20138.31905</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>0.5137058423</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>0.4907014254</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>0.5572585237</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>63386.2862</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>54443.51796</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>203676.2478</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>500000</upper_boundary>
+ </top_of_climb_range>
+ <top_of_descent_range description="Flown range from takeoff to top of descent">
+ <value>4329735.435</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000000</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>0.4999014739</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>
+ </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>
+ <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>14004.22881</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>16.6911147</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>14004.228808373002</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.067576816</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.957580772</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>0.267784187</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.191436979</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.924669034</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>0.467145347</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.32358539</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.88671607</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>0.617001451</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.548621791</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.814819481</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>0.811634047</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.773360095</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.746964181</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>0.976318453</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>1.115421815</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.624593025</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>1.21146329</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>1.427740836</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.499674101</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>1.429827854</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>2.112564592</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.21769763</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>1.867364888</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>2.599915253</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.174885536</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>1.971983901</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>3.420628612</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.083279283</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>2.113593806</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>4.164243156</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.041639641</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>2.167125385</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>5.130942918</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y 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>
+ </y>
+ </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>2.219197163</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>6.17200442</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y 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>
+ </y>
+ </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>2.227075627</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>6.172260794</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y 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>
+ </y>
+ </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>2.227075627</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>27.23273937</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y 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>
+ </y>
+ </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>2.227071912</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>27.22660641</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y 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>
+ </y>
+ </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>2.227071912</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>31.6198242</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y 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>
+ </y>
+ </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>1.736603193</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>32.46197422</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y 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>
+ </y>
+ </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>1.517243141</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>34.14627427</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y 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>
+ </y>
+ </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>0.939595006</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).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>37.08549195</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x 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>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>0.92429206</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </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>0.614104138</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>
+ <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>7717.542772675</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>386.68</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>157.909712567</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>286.170627658</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>105.8244264</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>391.995054058</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>612.814955814</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>347.40342</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>81.0</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>64.8</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>182.728</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>316.484166377</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>264.0</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>277.281530882</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>236.14919600000002</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>in_flight_entertainment</value>
+ </name>
+ <mass description="Mass of the fuselage operator item component.">
+ <value>81.0</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>total_fixed_galley_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="4" 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>1153.2</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>catering_mass</value>
+ </name>
+ <mass description="Mass of the fuselage operator item component.">
+ <value>846.24</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>5926.686035698</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>0.0</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>0.0</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>0.0</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>0.0</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>0.0</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>0.0</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>0.0</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>0.0</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>0.0</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>187.15636792302973</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>0.0</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>0.20624799999999996</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>124.77091194868649</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>26.723339999999997</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>8000</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>0.20624799999999996</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>62.385455974343245</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>13.361669999999998</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>
+ <wing>
+ <mass_properties description="mass_properties of component wing">
+ <mass description="component mass">
+ <value>5899.686597</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>16.97777054</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>-0.6705636773</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>13.15649787</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>-1.030445071</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>5.622599153</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>1.36425648</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</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>5.622599153</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>1.36425648</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</value>
+ </profile>
+ </section>
+ <section ID="2">
+ <chord_origin description="origin of chord (local)">
+ <x description="x coordinate of point">
+ <value>1.956243826</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>0.2585733096</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>-4.939499866</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>3.821246858</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>1.255091095</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</value>
+ </profile>
+ </section>
+ <section ID="3">
+ <chord_origin description="origin of chord (local)">
+ <x description="x coordinate of point">
+ <value>8.545130477</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>1.266923874</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>-16.46499955</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>0.9558418561</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>0.8293821242</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</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>-0.122907582</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>-0.122907582</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>-0.208453791</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>30.44658691</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>903.1495027</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>34.58488958</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>3.050854727</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>5.071328227</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>5.351645488</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>-6.608731805</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>1.344916246</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>
+ </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>2.348595458</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>-0.5869147714</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>3.22273277</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>3.523890414</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>0.4933838767</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>-5.639403513</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>0.9094551877</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>
+ </aerodynamic_surface>
+ </geometry>
+ </specific>
+ </empennage>
+ <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>13.15649787</value>
+ <unit>m</unit>
+ <lower_boundary>0</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>-1.030445071</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>0</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>-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>1.124519831</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>1.983993414</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>0</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>1.010691405</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Centroid in y-direction with regard to the local reference point.">
+ <value>2.452697049</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>0.341108349</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>1.19652444e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <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>0.759050885655</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>2.2490396612</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>1.956243826</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>-0.101697149</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>2.955506452</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>0.51586832583</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>1.5284987431999997</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>1.956243826</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>1.022822681</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>4.939499866</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>0</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>0.695636688</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Centroid in y-direction with regard to the local reference point.">
+ <value>-5.232975698</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>0.234777382</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>1.319256243e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <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>0.51586832583</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>1.5284987431999997</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>6.4287401</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>0.328341364</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>-18.569499866</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>0.22406712114432425</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>0.6639025811683681</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>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>1.124519831</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>-1.983993414</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>0</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>1.010691405</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Centroid in y-direction with regard to the local reference point.">
+ <value>-2.452697049</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>0.341108349</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>1.19652444e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <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>0.759050885655</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>2.2490396612</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>1.956243826</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>-0.101697149</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>-2.955506452</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>0.51586832583</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>1.5284987431999997</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>1.956243826</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>1.022822681</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>-4.939499866</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>0</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>0.695636688</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Centroid in y-direction with regard to the local reference point.">
+ <value>5.232975698</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>0.234777382</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>1.319256243e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <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>0.51586832583</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>1.5284987431999997</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>6.4287401</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>0.328341364</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>18.569499866</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>0.22406712114432425</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>0.6639025811683681</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>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>1.124519831</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>0</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>1.124519831</value>
+ <unit>m</unit>
+ <lower_boundary>0</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>2.167864117e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <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>0.759050885655</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>2.2490396612</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>0.759050885655</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>2.2490396612</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>
+ <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>8163.723809</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>291227.1488</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>9415.034095</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>293993.4407</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>-9.734017667</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>1640.24539</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>-9.734017667</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>-10.88764113</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>1640.24539</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>-10.88764113</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>14.88163757</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>0.00753679453</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>-2.361935723</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>2.117450668</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>2.117450668</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>0.8175031883</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>2.646813335</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>2.646813335</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>2.452509565</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>2.646813335</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>2.646813335</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>3.270012753</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>2.117450668</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>2.117450668</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>1021.17164</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>41.37265694</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>42.89384826</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>42.93889432</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>-8.648443839e-05</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>-0.01261898096</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>-8.648443839e-05</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>-0.005393592727</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>-0.01261898096</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>-0.005393592727</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>14.72478543</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>-5.893109505</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>-2.538575351</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>-1.058725334</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</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>1.296564592e-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>-1.058725334</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>3.270012753</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>2.585343883</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>2.268988035e-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>-1.852769335</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>3.270012753</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>495.2910093</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>0.4759428482</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>10.28599176</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>10.0164363</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>-0.04149876619</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>1.188151703</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>-0.04149876619</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>-0.00425818292</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>1.188151703</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>-0.00425818292</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>16.01745737</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>-5.923235836</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>-1.082828016</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>13.08977905</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>-5.923235836</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>-2.538575351</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>2565.399255</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>1437.777157</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>3004.86955</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>3004.86955</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>14.72478543</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>-5.923235836</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>-2.538575351</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>109167.0872</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>0.9064775155</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>18391.6134</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>1.407077304e-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>
+ <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>2.117450668</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>2.117450668</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>0.8175031883</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>2.646813335</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>2.646813335</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>2.452509565</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>2.646813335</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>2.646813335</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>3.270012753</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>2.117450668</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>2.117450668</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>1021.17164</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>41.37265694</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>42.89384826</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>42.93889432</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>-8.648443839e-05</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>-0.01261898096</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>-8.648443839e-05</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>-0.005393592727</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>-0.01261898096</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>-0.005393592727</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>14.72478543</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>5.953362166</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>-2.538575351</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>-1.058725334</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</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>1.296564592e-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>-1.058725334</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>3.270012753</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>2.585343883</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>2.268988035e-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>-1.852769335</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>3.270012753</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>495.2910093</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>0.4759428482</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>10.28599176</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>10.0164363</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>-0.04149876619</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>1.188151703</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>-0.04149876619</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>-0.00425818292</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>1.188151703</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>-0.00425818292</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>16.01745737</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>5.923235836</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>-1.082828016</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>13.08977905</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>5.923235836</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>-2.538575351</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>2565.399255</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>1437.777157</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>3004.86955</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>3004.86955</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>14.72478543</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>5.923235836</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>-2.538575351</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>109167.0872</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>0.9064775155</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>18391.6134</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>1.407077304e-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>
+ <landing_gear description="Geometric description of the aircraft undercarriage." tool_level="1">
+ <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>2558.0104</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>18.9592</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>-1.5956</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>[45.9, 40.2, 36.7, 35.3]</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>5.8</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>-1.4712</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>393.4109</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>-13.8761</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>0.1244</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>1.4339</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>-1.4339</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>-1.4339</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>21.4812</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>3.6161</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>-0.906</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>1082.2998</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>1.5224</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>3.6161</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>0.2491</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>1.9991</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>APS01347-A</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>-1.9991</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>APS01347-A</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>-1.9991</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>21.4812</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>-3.6161</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>-0.906</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>1082.2998</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>1.5224</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>3.6161</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>0.2491</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>1.9991</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>APS01347-A</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>-1.9991</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>APS01347-A</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>-1.9991</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>
+ <systems>
+ <mass_properties description="mass_properties of component systems">
+ <mass description="component mass">
+ <value>4825.986695</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>7.051442313</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>220.32</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>2.811299577</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>0</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>16.97777054</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>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </fuel_system>
+ <de_icing description="mass of ATA-30">
+ <value>31.34460331</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </de_icing>
+ <lighting description="mass of ATA-33">
+ <value>198.0485566</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </lighting>
+ <fire_protection description="mass of ATA-26">
+ <value>68.59844962</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </fire_protection>
+ <oxygen_system description="mass of ATA-35">
+ <value>91.34304</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </oxygen_system>
+ <flight_controls description="mass of ATA-27">
+ <value>1132.081306</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </flight_controls>
+ <instruments description="mass of ATA31">
+ <value>67.91403844</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </instruments>
+ <automatic_flight_system description="mass of ATA22">
+ <value>110.3603125</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </automatic_flight_system>
+ <navigation description="mass of ATA34">
+ <value>449.9305047</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </navigation>
+ <communication description="mass of ATA23">
+ <value>220.7206249</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </communication>
+ <bleed_air_system description="mass of ATA-36">
+ <value>170.9024353</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>133.6948041</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </hydraulic_generation>
+ <hydraulic_distribution description="mass of ATA-29">
+ <value>506.8091903</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </hydraulic_distribution>
+ <electrical_generation description="mass of ATA-24">
+ <value>517.834438</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </electrical_generation>
+ <electrical_distribution description="mass of ATA-24">
+ <value>437.5675573</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>164.6397078</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>303.8771255</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>249540.7594</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>1.971020666</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>55719.8203</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>0.9372327978</value>
+ <unit>W</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </average_bleed_air_demand>
+ </specific>
+ </systems>
+ </component_design>
+ <sizing_point>
+ <thrust_to_weight description="Total thrust (kN) divided by maximum aircraft weight (kN)">
+ <value>0.341170989</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </thrust_to_weight>
+ <wing_loading description="Maximum takeoff mass (MTOM) divided by wing area (Sref)">
+ <value>619.8444758</value>
+ <unit>kg/m^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </wing_loading>
+ </sizing_point>
+ <assessment description="Assessment data">
+ <performance description="Assessment of performance values">
+ <takeoff>
+ <takeoff_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>1714.684647</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </takeoff_distance_normal_safety>
+ </takeoff>
+ <landing>
+ <needed_runway_length description="Needed runway length with all engines operating and maximum landing mass">
+ <value>1293.066314</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </needed_runway_length>
+ </landing>
+ </performance>
+ </assessment>
+</aircraft_exchange_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/routes/settings/+page.svelte b/UnicadoGUI/Frontend/src/routes/settings/+page.svelte
index 85503ea5..a2cf8d48 100644
--- a/UnicadoGUI/Frontend/src/routes/settings/+page.svelte
+++ b/UnicadoGUI/Frontend/src/routes/settings/+page.svelte
@@ -10,8 +10,10 @@
Input,
Styles,
TabContent,
- TabPane
+ TabPane,
+ Tooltip
} from "@sveltestrap/sveltestrap";
+ import {onMount} from "svelte";
let changed = false;
class EnergyCarrier{
@@ -81,7 +83,258 @@
}
}
+ onMount(async () => {
+ await getModuleConf();
+ })
+
+ async function getModuleConf() {
+ try {
+ const res = await fetch(`http://127.0.0.1:8000/projects/aircraft_exchange_file/`);
+ const data = await res.json();
+ modalModule.name = 'exchange_file';
+ modalModule.response = JSON.parse(data);
+ modalModule.html = [];
+ generateHTML(modalModule.response);
+ } catch (error) {
+ console.error(error);
+ modalModule.name = "no";
+ modalModule.response = {};
+ modalModule.html = [];
+ modalModule.html.push(new SettingsLabel("No config found!"));
+ }
+ }
+
+/**
+ * TODO: make it more modula, as now 2 files have a lot same code
+*/
+type dictionary = {
+ [key: string]: any
+ }
+ /* Dictionary with information of the module
+ * including the json response and the settings elements it needs to implement in the dom
+ */
+ let modalModule: dictionary = {
+ name: '',
+ response: {},
+ html: []
+ }
+
+ //check if string is a number
+ function isNumber(n:string){
+ return!isNaN(parseFloat(n))&&isFinite(parseFloat(n))
+ }
+
+ //Interface for Ui-elements in module settings and it's implementations
+ interface SettingsUi {
+ type: string;
+ label: string;
+ description: string;
+ bind: string;
+ }
+
+ class SettingsSwitch implements SettingsUi {
+ readonly type = "switch";
+ label: string;
+ description: string;
+ bind: string;
+
+ constructor(label: string, description: string, bind: string) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ }
+ }
+
+ class SettingsSelector implements SettingsUi {
+ readonly type = "selector";
+ label: string;
+ description: string;
+ bind: string;
+ options: string[];
+
+ constructor(label: string, description: string, bind: string, options: string[]) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ this.options = options;
+ }
+ }
+
+ class SettingsTextfield implements SettingsUi {
+ readonly type = "textfield";
+ label: string;
+ description: string;
+ bind: string;
+ input: string;
+
+ constructor(label: string, description: string, bind: string, input: string) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ this.input = input;
+ }
+ }
+
+ class SettingsNumberfield implements SettingsUi {
+ readonly type = "numberfield";
+ label: string;
+ description: string;
+ bind: string;
+ unit: string = '-';
+ max: number = Number.POSITIVE_INFINITY;
+ min: number = Number.NEGATIVE_INFINITY;
+
+ constructor(label: string, description: string, bind: string) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ }
+ setMax(max:number){
+ this.max=max;
+ }
+ setMin(min:number){
+ this.min=min;
+ }
+ setUnit(unit:string){
+ this.unit=unit;
+ }
+ }
+
+ class SettingsLabel {
+ readonly type = "label";
+ label: string;
+
+ constructor(label: string) {
+ this.label = label;
+ }
+ }
+ /*Parse json response to matching SettingsUi-Elements
+ * to portray it later in the DOM
+ * recursive Function
+ * */
+ function generateHTML(json: dictionary) {
+ Object.entries(json).forEach(([key, value]) => {
+ if (value == null) {
+ return
+ }
+ if (value.hasOwnProperty("value")) {
+ if (value["@description"] && value["@description"].toLowerCase().includes("switch")) {
+ value.value = (value.value === 'true' || value.value === "1") //transform string input to boolean for easier binding
+ modalModule.html.push(new SettingsSwitch(key, value["@description"], value))
+ } else if (value["@description"] && value["@description"].toLowerCase().includes("selector")) {
+ let options = [];
+ for (let i = 0; i < 5; i++) {
+ if (value["@description"].includes("mode_" + i)) {
+ options.push("mode_" + i)
+ }
+ }
+ modalModule.html.push(new SettingsSelector(key, value["@description"], value, options))
+ }else if(isNumber(value.value)){
+ value.value=parseFloat(value.value);
+ let numberField = new SettingsNumberfield(key, value["@description"], value)
+ if(value.hasOwnProperty('lower_boundary')&&isNumber(value['lower_boundary'])){numberField.setMin(value['lower_boundary'])}
+ if(value.hasOwnProperty('upper_boundary')&&isNumber(value['upper_boundary'])){numberField.setMax(value['upper_boundary'])}
+ if(value.hasOwnProperty("@unit")){numberField.setUnit(value["@unit"])}//spaeter entweder unit oder Unit in XML
+ if(value.hasOwnProperty("@Unit")){numberField.setUnit(value["@Unit"])}
+ if(value.hasOwnProperty("unit")){numberField.setUnit(value["unit"])}
+ if(value.hasOwnProperty("Unit")){numberField.setUnit(value["Unit"])}
+ modalModule.html.push(numberField);
+ } else {
+ modalModule.html.push(new SettingsTextfield(key, value["@description"], value, key))
+ }
+ } else if (typeof value === "object") {
+ modalModule.html.push(new SettingsLabel(key))
+ generateHTML(json[key])
+ } else {
+ return;
+ }
+ })
+ }
+
+ //Replacing underscores to space
+ function formatLabel(label: string) {
+ return label.replaceAll("_", " ")
+ }
+ //check if the settings modal of a module changed
+ function checkModalChanged() {
+ modalChanged = true;
+ modalChanged = modalChanged;
+ }
+
+ let modalChanged: boolean = false;
+
+ //check if number is in boundry
+ function validateNumber(index:number){
+ console.log("validateNumber")
+ if(modalModule.html[index].bind.value<modalModule.html[index].min){
+ modalModule.html[index].bind.value=modalModule.html[index].min;
+ }else if(modalModule.html[index].bind.value>modalModule.html[index].max){
+ modalModule.html[index].bind.value=modalModule.html[index].max;
+ }
+ }
+
+ //Calculate Stepsize of number inputs from current value
+ function calcStepSize(value:number){
+ const numberString = value.toString()
+ if (!numberString.includes('.')) {
+ return 1;
+ } else {
+ const decimalPart = numberString.split('.')[1];
+ return Math.pow(10, -decimalPart.length);
+ }
+ }
</script>
+{#each modalModule.html as element, index}
+{#if element.type == "switch"}
+ <Input id="uiElement{index}" type="switch" label="{formatLabel(element.label)}"
+ bind:checked={element.bind.value} on:change={()=>checkModalChanged()}/>
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+{:else if element.type == "label"}
+ <h3>{formatLabel(element.label)}</h3>
+{:else if element.type == "selector"}
+ <h6>{formatLabel(element.label)}</h6>
+ <Input id="uiElement{index}" type="select" bind:value={element.bind.value}
+ on:change={()=>checkModalChanged()}>
+ {#each element.options as option}
+ <option>{option}</option>
+ {/each}
+ </Input>
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+{:else if element.type == "textfield"}
+ <h7>{formatLabel(element.label)}</h7>
+ <Input id="uiElement{index}" type="text" bind:value={element.bind.value}
+ on:change={()=>checkModalChanged()}/>
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+{:else if element.type == "numberfield"}
+ {#if element.unit != "1" && element.unit != "-" && element.unit != "count"}
+ <h7>{formatLabel(element.label)} (in {element.unit})</h7>
+ {:else}
+ <h7>{formatLabel(element.label)}</h7>
+ {/if}
+ {#if element.max != Number.POSITIVE_INFINITY && element.min != Number.NEGATIVE_INFINITY}
+ <Input type="range" min={element.min} max={element.max} step=0.01 bind:value={element.bind.value}
+ placeholder="range placeholder" on:change={()=>checkModalChanged()}/>
+ <Input id="uiElement{index}" type="number" min={element.min} max={element.max} step=0.01
+ bind:value={element.bind.value} on:change={()=>checkModalChanged()} on:blur={()=>validateNumber(index)}/>
+ {:else}
+ <Input id="uiElement{index}" type="number" min={element.min} max={element.max} step={calcStepSize(element.bind.value)}
+ bind:value={element.bind.value} on:change={()=>checkModalChanged()} on:blur={()=>validateNumber(index)}/>
+ {/if}
+
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+{/if}
+{/each}
+<!--
+
+
<h1>Aircraftmodelsettings</h1>
<ButtonGroup style="margin-bottom: 20px">
<Button color="dark" outline ><Icon name="bootstrap-reboot"/> Reset </Button>
@@ -135,12 +388,7 @@
<option value="high">high</option>
</Input>
</FormGroup>
- <!-- <FormGroup floating label="Definitions for empennage design">-->
- <!-- <Input type="select" placeholder="Enter a value">-->
- <!-- <option value="low">low</option>-->
- <!-- <option value="mid">mid</option>-->
- <!-- </Input>-->
- <!-- </FormGroup>-->
+
<h5>Design description of the undercarriage</h5>
<FormGroup floating label="Mounting position of the main landing gear">
@@ -338,6 +586,7 @@
</Form>
+-->
<Styles/>
\ No newline at end of file
--
GitLab