<aircraft_exchange_file>
<requirements_and_specifications description="Requirements and specifications">
<general description="General aircraft information">
<type description="Aircraft type">
<value>UNICADO</value>
</type>
<model description="Model - Version">
<value>SMR-180-TF</value>
</model>
</general>
<mission_files description="Name of xml files which are located in the mission_data directory and contain the flight phase data" tool_level="0">
<design_mission_file description="Name of the design mission xml">
<value>design_mission.xml</value>
</design_mission_file>
<study_mission_file description="Name of the study mission xml">
<value>study_mission.xml</value>
</study_mission_file>
<requirements_mission_file description="Name of the requirements mission xml">
<value>requirements_mission.xml</value>
</requirements_mission_file>
</mission_files>
<design_specification description="Design specification">
<configuration description="Configuration information">
<configuration_type description="Aircraft configuration. Selector: tube_and_wing">
<value>tube_and_wing</value>
</configuration_type>
<fuselage_definition description="Design description of the fuselage.">
<fuselage_type description="Fuselage type. Selector: single_aisle / wide_body">
<value>single_aisle</value>
</fuselage_type>
<fuselage_pressurization description="Switch to enable pressurized fuselage. Switch: true (On) / false (Off)">
<value>true</value>
</fuselage_pressurization>
</fuselage_definition>
<wing_definition description="Definitions for wing design">
<mounting description="Wing mounting. Selector: low">
<value>low</value>
</mounting>
</wing_definition>
<empennage_definition description="Definitions for empennage design">
<empennage_type description="Empennage type. Selector: conventional">
<value>conventional</value>
</empennage_type>
</empennage_definition>
<undercarriage_definition description="Design description of the undercarriage.">
<main_gear_mounting description="Mounting position of the main landing gear. Selector: wing_mounted">
<value>wing_mounted</value>
</main_gear_mounting>
<undercarriage_retractability description="Set retractability of landing gear. Selector: retractable / non_retractable">
<value>retractable</value>
</undercarriage_retractability>
</undercarriage_definition>
<tank_definition description="Energy tanks information">
<tank ID="0" description="Inner left tank">
<energy_carrier_ID description="see energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
<location description="Component where the tank is located. Selector: fuselage / wing / horizontal_stabilizer">
<value>fuselage</value>
</location>
<position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
<value>tail_cone</value>
</position>
<energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
<value>0.0</value>
<unit>1</unit>
<lower_boundary>0.0</lower_boundary>
<upper_boundary>1.0</upper_boundary>
</energy_share>
</tank>
<tank ID="1" description="Outer left tank">
<energy_carrier_ID description="see energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
<location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
<value>fuselage</value>
</location>
<position description="Position of tank in location. Selector: center / inner_left / outer_left / inner_right / outer_right / total">
<value>rear</value>
</position>
<energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Equals 0.0 for kerosene tanks. Only relevant for liquid hydrogen (not impemented yet). ">
<value>0.0</value>
<unit>1</unit>
<lower_boundary>0.0</lower_boundary>
<upper_boundary>1.0</upper_boundary>
</energy_share>
</tank>
</tank_definition>
<loads description="Loads information">
<design_load_factor description="Design load factor n">
<maximum description="Maximum design load factor n">
<value>2.5</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>4</upper_boundary>
</maximum>
<minimum description="Minimum design load factor n">
<value>-1.0</value>
<unit>1</unit>
<lower_boundary>-2.0</lower_boundary>
<upper_boundary>0.0</upper_boundary>
</minimum>
<maneuver description="Standard maneuver load factor for e.g. flare">
<value>1.1</value>
<unit>1</unit>
<lower_boundary>0.0</lower_boundary>
<upper_boundary>2.0</upper_boundary>
</maneuver>
</design_load_factor>
</loads>
<aerodynamic_technologies description="Integration of aerodynamic technologies on the aircraft: Switch: false (no additional aerodynamic technologies are considered)">
<value>false</value>
</aerodynamic_technologies>
</configuration>
<transport_task description="Define the transport task for aircraft project.">
<passenger_definition description="Define the masses of the passengers">
<total_number_passengers description="Design number of passengers">
<value>180</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1000</upper_boundary>
</total_number_passengers>
<mass_per_passenger description="Design mass of a single passenger WITHOUT luggage">
<value>80</value>
<unit>kg</unit>
<lower_boundary>50</lower_boundary>
<upper_boundary>200</upper_boundary>
</mass_per_passenger>
<luggage_mass_per_passenger description="Design mass of the luggage for a single passenger">
<value>15</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>25</upper_boundary>
</luggage_mass_per_passenger>
</passenger_definition>
<multi_passenger_deck_layout description="Switch to select a multi passenger deck fuselage design. Switch: false (Off)">
<value>false</value>
<default>false</default>
<specific_number_of_passenger_decks>
<value>2</value>
<unit>-</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>3</upper_boundary>
<default>2</default>
</specific_number_of_passenger_decks>
</multi_passenger_deck_layout>
<passenger_class_definition>
<class_distribution description="Relative passenger distribution for the classes: President Class/First Class/Business Class/Premium Economy/Economy. Sum must be equal to 1!">
<value>0/0/0/0/1</value>
</class_distribution>
</passenger_class_definition>
<cargo_definition description="Definition of cargo which does not belong to passengers">
<additional_cargo_mass description="Mass of cargo which does not belong to passengers">
<value>2200</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>25000</upper_boundary>
</additional_cargo_mass>
<cargo_density description="Density of cargo which does not belong to passengers">
<value>165</value>
<unit>kg/m^3</unit>
<lower_boundary>150</lower_boundary>
<upper_boundary>200</upper_boundary>
</cargo_density>
</cargo_definition>
</transport_task>
<energy_carriers description="Energy carriers information">
<energy_carrier ID="0" description="One specific energy carrier">
<type description="Energy type (for multifuel engine create new ID). Selector: kerosene">
<value>liquid_hydrogen</value>
</type>
<density description="Energy carrier density.">
<value>70.79</value>
<unit>kg/m^3</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10000</upper_boundary>
</density>
</energy_carrier>
</energy_carriers>
<propulsion description="Propulsion information">
<propulsor ID="0" description="Information for specific propulsor">
<powertrain description="Way the power is generated from the source. Selector: turbo">
<value>turbo</value>
</powertrain>
<type description="Type of main thrust generator. Selector: fan">
<value>fan</value>
</type>
<position description="Propulsor position (arrangement order acc to ID order)">
<parent_component description="Position on component. Selector: wing / fuselage / empennage">
<value>wing</value>
</parent_component>
<x description="X-position (aircraft coordinate system). Selector: front / back">
<value>front</value>
</x>
<y description="Y-position (aircraft coordinate system). Selector: left / right">
<value>left</value>
</y>
<z description="Z-position (aircraft coordinate system). Selector: over / mid / under / in">
<value>under</value>
</z>
</position>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
<thrust_share description="Share of this thrust in relation to required aircraft thrust">
<value>0.5</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</thrust_share>
</propulsor>
<propulsor ID="1" description="Information for specific propulsor">
<powertrain description="Way the power is generated from the source. Selector: turbo">
<value>turbo</value>
</powertrain>
<type description="Type of main thrust generator. Selector: fan">
<value>fan</value>
</type>
<position description="Propulsor position (arrangement order acc to ID order)">
<parent_component description="Position on component. Selector: wing / fuselage / empennage">
<value>wing</value>
</parent_component>
<x description="X-position (aircraft coordinate system). Selector: front / back">
<value>front</value>
</x>
<y description="Y-position (aircraft coordinate system). Selector: left / right">
<value>right</value>
</y>
<z description="Z-position (aircraft coordinate system). Selector: over / mid / under / in">
<value>under</value>
</z>
</position>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
<thrust_share description="Share of this thrust in relation to required aircraft thrust">
<value>0.5</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</thrust_share>
</propulsor>
<energy_provider description="Source where energy is coming from per segment">
<ground description="Source where energy is coming from in the ground mission segment">
<energy_carrier_ID description="see energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</ground>
<taxi description="source where energy is coming from in the taxi mission segment">
<energy_carrier_ID description="see energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</taxi>
<takeoff description="source where energy is coming from in the takeoff mission segment">
<energy_carrier_ID description="see energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</takeoff>
<climb description="source where energy is coming from in the climb mission segment">
<energy_carrier_ID description="see energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</climb>
<cruise description="source where energy is coming from in the cruise mission segment">
<energy_carrier_ID description="see energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</cruise>
<descent description="source where energy is coming from in the descent mission segment">
<energy_carrier_ID description="see energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</descent>
<landing description="source where energy is coming from in the landing mission segment">
<energy_carrier_ID description="see energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</landing>
</energy_provider>
</propulsion>
<technology>
<variable_camber description="Switch if variable camber is used. Switch: false (Off)">
<value>false</value>
</variable_camber>
</technology>
</design_specification>
<requirements description="Aircraft design requirements">
<top_level_aircraft_requirements description="Top level aircraft requirements (TLAR)">
<maximum_structrual_payload_mass description="Maximum payload mass which can be carried by the aircraft (e.g. for short trips)">
<value>19300</value>
<unit>kg</unit>
<lower_boundary>100</lower_boundary>
<upper_boundary>150000</upper_boundary>
</maximum_structrual_payload_mass>
<takeoff_distance description="Design takeoff distance (Balanced Field Length) at Sea Level with maximum takeoff mass (MTOM) and (ISA + deltaISA)-Conditions">
<value>1951</value>
<unit>m</unit>
<lower_boundary>600</lower_boundary>
<upper_boundary>5000</upper_boundary>
</takeoff_distance>
<landing_field_length description="Needed runway length at Sea Level with maximum landing mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)">
<value>2425.67</value>
<unit>m</unit>
<lower_boundary>600</lower_boundary>
<upper_boundary>5000</upper_boundary>
</landing_field_length>
<icao_aerodrome_reference_code description="ICAO reference code - code_number 1-4 (field length) + code_letter A-F (wing span limits) + faa ADG code number I-VI (wing span limits + tail height limits) + Aircraft Approach Category letter A-D">
<value>3CIIIC</value>
</icao_aerodrome_reference_code>
<flight_envelope description="Maxima of design flight envelope">
<maximum_operating_mach_number description="Maximum operating mach number">
<value>0.82</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</maximum_operating_mach_number>
<maximum_operating_velocity description="Maximum operating speed (maximum dynamic pressure)">
<value>180</value>
<unit>m/s</unit>
<lower_boundary>50</lower_boundary>
<upper_boundary>250</upper_boundary>
</maximum_operating_velocity>
<maximum_approach_speed description="Maximum allowed approach speed.">
<value>67.65</value>
<unit>m/s</unit>
<lower_boundary>50</lower_boundary>
<upper_boundary>90</upper_boundary>
</maximum_approach_speed>
<maximum_operating_altitude description="Maximum operating altitude">
<value>12192</value>
<unit>m</unit>
<lower_boundary>4500</lower_boundary>
<upper_boundary>20000</upper_boundary>
</maximum_operating_altitude>
<maximum_altitude_one_engine_inoperative description="Maximum operating altitude with one engine inoperative">
<value>4572</value>
<unit>m</unit>
<lower_boundary>1500</lower_boundary>
<upper_boundary>12000</upper_boundary>
</maximum_altitude_one_engine_inoperative>
<climb_or_descent_segment_gradient description="climb / descent segment gradient">
<value>0.024</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</climb_or_descent_segment_gradient>
</flight_envelope>
<pavement_classification_number description="Runway pavement classification number (PCN) - limits the maximum allowed aircraft classification number of undercarriage">
<value>55</value>
<unit>1</unit>
<lower_boundary>5</lower_boundary>
<upper_boundary>120</upper_boundary>
</pavement_classification_number>
<design_mission description="Requirements regarding the design mission">
<delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
<value>0</value>
<unit>K</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</delta_ISA>
<range description="Target range for design mission">
<value>4537400</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>20000000</upper_boundary>
</range>
<contingency description="Contingency fuel in percentage (reserve fuel)">
<value>0.06</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>0.08</upper_boundary>
</contingency>
<alt_dist description="Alternate distance in m (reserve fuel)">
<value>370400</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>926000</upper_boundary>
</alt_dist>
<loiter_time description="Loiter time in seconds (reserve fuel)">
<value>1800</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>3600</upper_boundary>
</loiter_time>
<initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise">
<value>0.78</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</initial_cruise_mach_number>
<initial_cruise_altitude description="Initial cruise altitude (ICA) at top of descent. May be altered during cruise">
<value>10058.4</value>
<unit>m</unit>
<lower_boundary>1000</lower_boundary>
<upper_boundary>20000</upper_boundary>
</initial_cruise_altitude>
<climb_speed_schedule description="Climb speed for different altitudes">
<climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
<value>128.6112</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>250</upper_boundary>
</climb_speed_below_FL100>
<climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
<value>154.3334</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>250</upper_boundary>
</climb_speed_above_FL100>
<delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
<value>-0.02</value>
<unit>1</unit>
<lower_boundary>-0.3</lower_boundary>
<upper_boundary>0.01</upper_boundary>
</delta_mach_climb_cruise>
</climb_speed_schedule>
<descent_speed_schedule description="Descent speed for different altitudes">
<descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
<value>128.6112</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>250</upper_boundary>
</descent_speed_below_FL100>
<descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
<value>154.3334</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>250</upper_boundary>
</descent_speed_above_FL100>
</descent_speed_schedule>
<time_to_climb description="Time the aircraft takes to climb to cruise altitude">
<value>2100</value>
<unit>s</unit>
<lower_boundary>600</lower_boundary>
<upper_boundary>3600</upper_boundary>
</time_to_climb>
<fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
<fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)">
<value>mode_0</value>
</fuel_estimation_selector>
</fuel_planning>
</design_mission>
<study_mission description="Requirements regarding the study mission">
<delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
<value>0</value>
<unit>K</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</delta_ISA>
<range description="Target range for the study mission">
<value>1481600</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>20000000</upper_boundary>
</range>
<initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise">
<value>0.78</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</initial_cruise_mach_number>
<initial_cruise_altitude description="Initial cruise altitude at top of descent. May be altered during cruise">
<value>10668</value>
<unit>m</unit>
<lower_boundary>1000</lower_boundary>
<upper_boundary>20000</upper_boundary>
</initial_cruise_altitude>
<climb_speed_schedule description="Climb speed for different altitudes">
<climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
<value>128.6112</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>250</upper_boundary>
</climb_speed_below_FL100>
<climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
<value>154.3334</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>250</upper_boundary>
</climb_speed_above_FL100>
<delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
<value>-0.02</value>
<unit>1</unit>
<lower_boundary>-0.3</lower_boundary>
<upper_boundary>0.01</upper_boundary>
</delta_mach_climb_cruise>
</climb_speed_schedule>
<descent_speed_schedule description="Descent speed for different altitudes">
<descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
<value>128.6112</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>250</upper_boundary>
</descent_speed_below_FL100>
<descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
<value>154.3334</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>250</upper_boundary>
</descent_speed_above_FL100>
</descent_speed_schedule>
<fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
<fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)">
<value>mode_0</value>
</fuel_estimation_selector>
</fuel_planning>
<payload_fractions description="Set the fraction of different design payload values for the study mission">
<cargo_fraction description="Fraction of the design cargo mass which is used for the study mission">
<value>0.75</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</cargo_fraction>
<passenger_mass_fraction description="Fraction of the design passenger mass which is used for the study mission">
<value>0.75</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</passenger_mass_fraction>
</payload_fractions>
</study_mission>
</top_level_aircraft_requirements>
<additional_requirements description="Additional requirements">
<landing_gear description="Landing gear requirements and operational conditions">
<friction_coefficient description="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">
<value>0.03</value>
<default>0.03</default>
<unit>1</unit>
<lower_boundary>0.02</lower_boundary>
<upper_boundary>0.08</upper_boundary>
</friction_coefficient>
<braking_coefficient description="Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189">
<value>0.34189</value>
<default>0.34189</default>
<unit>1</unit>
<lower_boundary>0.06</lower_boundary>
<upper_boundary>0.5</upper_boundary>
</braking_coefficient>
</landing_gear>
</additional_requirements>
</requirements>
<assessment_scenario description="Scenario for ecological and economical assessment">
<flights_per_year description="Number of flights per year">
<value>2227</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>4000</upper_boundary>
</flights_per_year>
<duration_operation description="Operating years of aircraft">
<value>25</value>
<unit>a</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>50</upper_boundary>
</duration_operation>
</assessment_scenario>
</requirements_and_specifications>
<analysis>
<masses_cg_inertia description="Masses, Center of Gravity, Inertias." tool_level="3">
<maximum_takeoff_mass description="MTOM">
<mass_properties description="maximum takeoff mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>1452317.8298</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>5883140.3113</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>6648774.9188</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>21.5717</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>-0.5183</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>75000.4477</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</maximum_takeoff_mass>
<operating_mass_empty description="OME">
<mass_properties description="operating mass empty properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>970318.8048</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>3930628.3776</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>4442162.1769</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>19.9824</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>-0.687</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>50109.1037</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</operating_mass_empty>
<manufacturer_mass_empty description="MME">
<mass_properties description="manufacturer mass empty properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>890205.4692</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>3606100.2443</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>4075399.8019</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>19.9343</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>-0.7488</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>45971.8991</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</manufacturer_mass_empty>
<maximum_zero_fuel_mass description="MZFM">
<mass_properties description="maximum zero fuel mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>1344046.3619</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>5444547.4464</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>6153103.3751</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>20.4427</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>-0.5631</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>69409.1037</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</maximum_zero_fuel_mass>
<maximum_payload_mass description="">
<mass_properties description="maximum payload mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>21.6379</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>-0.2413</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>19300</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</maximum_payload_mass>
<maximum_landing_mass description="MLM">
<mass_properties description="maximum landing mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>1229364.0985</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>4979985.3288</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>5628082.9282</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>19.9824</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>-0.687</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>63486.6941</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</maximum_landing_mass>
<maximum_fuel_mass description="">
<mass_properties description="maximum fuel mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>35.5725</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>0.0365</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>5651.1479</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</maximum_fuel_mass>
<ferry_range_mass description="">
<mass_properties description="ferry range mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>21.5624</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>-0.6137</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>55760.2516</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</ferry_range_mass>
<most_forward_mass description="">
<mass_properties description="most forward mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>970318.8048</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>3930628.3776</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>4442162.1769</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>19.4898</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>70489.3705</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</most_forward_mass>
<most_afterward_mass description="">
<mass_properties description="most afterward mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>970318.8048</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>3930628.3776</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>4442162.1769</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>21.7832</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>60020.4477</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</most_afterward_mass>
<design_mass description="">
<mass_properties description="design mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>1452317.8298</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>5883140.3113</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>6648774.9188</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>21.5717</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>-0.5183</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>75000.4477</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</design_mass>
<design_fuel_mass description="">
<mass_properties description="design fuel mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity w.r.t global coordinate system.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>35.5866</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>0.0369</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
<mass description="Mass">
<value>5591.344</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
</mass_properties>
</design_fuel_mass>
</masses_cg_inertia>
<aerodynamics description="Aerodynamical analysis" tool_level="3">
<polar>
<polar_file description="Name of polar file">
<value>SMR-180-TF_design_trimmed_polar.xml</value>
</polar_file>
<configurations description="Number of configurations in the polar file">
<value>7</value>
<unit>1</unit>
<lower_boundary>-2147483648</lower_boundary>
<upper_boundary>2147483647</upper_boundary>
</configurations>
<configuration ID="0" description="Configuration in polar file marked with ID - name can vary">
<type description=" Type">
<value>cruise</value>
</type>
<name description=" Name">
<value>clean</value>
</name>
</configuration>
<configuration ID="1" description="Configuration in polar file marked with ID - name can vary">
<type description=" Type">
<value>departure</value>
</type>
<name description=" Name">
<value>takeoff</value>
</name>
</configuration>
<configuration ID="2" description="Configuration in polar file marked with ID - name can vary">
<type description=" Type">
<value>departure</value>
</type>
<name description=" Name">
<value>takeoff_landing_gear_retracted</value>
</name>
</configuration>
<configuration ID="3" description="Configuration in polar file marked with ID - name can vary">
<type description=" Type">
<value>departure</value>
</type>
<name description=" Name">
<value>climb</value>
</name>
</configuration>
<configuration ID="4" description="Configuration in polar file marked with ID - name can vary">
<type description=" Type">
<value>approach</value>
</type>
<name description=" Name">
<value>approach</value>
</name>
</configuration>
<configuration ID="5" description="Configuration in polar file marked with ID - name can vary">
<type description=" Type">
<value>approach</value>
</type>
<name description=" Name">
<value>approach_landing_gear_out</value>
</name>
</configuration>
<configuration ID="6" description="Configuration in polar file marked with ID - name can vary">
<type description=" Type">
<value>approach</value>
</type>
<name description=" Name">
<value>landing</value>
</name>
</configuration>
</polar>
<reference_values>
<b description="Wing half span">
<value>35.68224296</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</b>
<MAC description="Mean aerodynamic chord">
<value>4.488507864</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</MAC>
<S_ref description="Wing reference area">
<value>134.0234172</value>
<unit>m^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</S_ref>
<neutral_point>
<x description="x component of neutral point">
<value>22.70357943</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
</neutral_point>
</reference_values>
<lift_coefficients>
<C_LoptimumCruise description="C_LoptimumCruise">
<value>0.632</value>
<unit>1</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</C_LoptimumCruise>
<C_LmaxLanding description="C_LmaxLanding">
<value>3.136</value>
<unit>1</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</C_LmaxLanding>
<C_LmaxT-O description="C_LmaxTO">
<value>2.681</value>
<unit>1</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</C_LmaxT-O>
<C_LgroundRoll description="C_LgroundRoll">
<value>0.4</value>
<unit>1</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</C_LgroundRoll>
</lift_coefficients>
<max_spoiler_factor description="max_spoiler_factor">
<value>2.5</value>
<unit>1</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</max_spoiler_factor>
</aerodynamics>
<mission description="Mission data" tool_level="0">
<design_mission description="Data of design mission">
<range description="Traveled range from break release to end of taxi at destination">
<value>4538384.063</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>20000000</upper_boundary>
</range>
<loaded_mission_energy description="Amount of energy loaded into tanks (including reserves) for the mission">
<mission_energy ID="0" description="Amount of energy loaded into tanks (including reserves) for specified energy carrier">
<consumed_energy description="Energy amount">
<value>6.783426413e+11</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</mission_energy>
</loaded_mission_energy>
<in_flight_energy description="Amount of energy needed for in-flight segments (all segments from takeoff to landing)">
<trip_energy ID="0" description="Amount of energy needed for trip segments (all segments from takeoff to landing) for specified energy carrier">
<consumed_energy description="Energy amount">
<value>5.41329264e+11</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</trip_energy>
<takeoff_energy ID="0" description="Amount of energy needed for takeoff segment for specified energy carrier">
<consumed_energy description="Energy amount">
<value>9026058430</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</takeoff_energy>
<landing_energy ID="0" description="Amount of energy needed for landing segment for specified energy carrier">
<consumed_energy description="Energy amount">
<value>7288548612</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</landing_energy>
</in_flight_energy>
<taxi_energy description="Amount of energy needed for taxiing specified energy carrier">
<taxi_out_energy ID="0" description="Amount of energy needed for taxiing at origin for specified energy carrier">
<consumed_energy description="Energy amount">
<value>7381362017</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</taxi_out_energy>
<taxi_in_energy ID="0" description="Amount of energy needed for taxiing at destination for specified energy carrier">
<consumed_energy description="Energy amount">
<value>4100756676</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</taxi_in_energy>
</taxi_energy>
<block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
<value>21017.79804</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>45000</upper_boundary>
</block_time>
<flight_time description="Flight time for the whole mission">
<value>20177.79804</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>44500</upper_boundary>
</flight_time>
<takeoff_engine_derate description="Engine power demand">
<value>1</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</takeoff_engine_derate>
<cruise description="Characteristics of the cruise segment">
<average_lift_coefficient description="Lift coefficient CL_average: Arithmetic mean over the entire cruise flight">
<value>0.497905048</value>
<unit>1</unit>
<lower_boundary>-0.01</lower_boundary>
<upper_boundary>1</upper_boundary>
</average_lift_coefficient>
<minimum_lift_coefficient description="Minimum cruise flight lift coefficient CL_min">
<value>0.4751027938</value>
<unit>1</unit>
<lower_boundary>-0.01</lower_boundary>
<upper_boundary>1</upper_boundary>
</minimum_lift_coefficient>
<maximum_lift_coefficient description="Maximum cruise flight lift coefficient CL_max">
<value>0.5212589617</value>
<unit>1</unit>
<lower_boundary>-0.01</lower_boundary>
<upper_boundary>1</upper_boundary>
</maximum_lift_coefficient>
<top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
<value>74418.20047</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>150000</upper_boundary>
</top_of_climb_mass>
<top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
<value>70543.5885</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>150000</upper_boundary>
</top_of_descent_mass>
<top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
<value>204794.9501</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>4537400</upper_boundary>
</top_of_climb_range>
<top_of_descent_range description="Flown range from takeoff to top of descent">
<value>4323225.176</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>4537400</upper_boundary>
</top_of_descent_range>
<cruise_steps description="Cruise step information">
<cruise_step ID="0" description="Data of a cruise step">
<relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
<value>0.4998879854</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</relative_end_of_cruise_step>
<altitude description="Altitude of cruise step">
<value>10058.40002</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>15000</upper_boundary>
</altitude>
</cruise_step>
<cruise_step ID="1" description="Data of a cruise step">
<relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
<value>1</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</relative_end_of_cruise_step>
<altitude description="Altitude of cruise step">
<value>10668.00002</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>15000</upper_boundary>
</altitude>
</cruise_step>
</cruise_steps>
</cruise>
</design_mission>
<study_mission description="Data of study mission">
<takeoff_mass description="Takeoff mass">
<value>67053.2029</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>300000</upper_boundary>
</takeoff_mass>
<range description="Traveled range from break release to end of taxi at destination">
<value>1482595.498</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>20000000</upper_boundary>
</range>
<loaded_mission_energy description="Amount of energy loaded into tanks (including reserves) for the mission">
<mission_energy ID="0" description="Amount of energy loaded into tanks (including reserves) for specified energy carrier">
<consumed_energy description="Energy amount">
<value>3.034939615e+11</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</mission_energy>
</loaded_mission_energy>
<in_flight_energy description="Amount of energy needed for in-flight segments (all segments from takeoff to landing)">
<trip_energy ID="0" description="Amount of energy needed for trip segments (all segments from takeoff to landing) for specified energy carrier">
<consumed_energy description="Energy amount">
<value>1.796191547e+11</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</trip_energy>
<takeoff_energy ID="0" description="Amount of energy needed for takeoff segment for specified energy carrier">
<consumed_energy description="Energy amount">
<value>7717278972</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</takeoff_energy>
<landing_energy ID="0" description="Amount of energy needed for landing segment for specified energy carrier">
<consumed_energy description="Energy amount">
<value>6881012278</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</landing_energy>
</in_flight_energy>
<taxi_energy description="Amount of energy needed for taxiing specified energy carrier">
<taxi_out_energy ID="0" description="Amount of energy needed for taxiing at origin for specified energy carrier">
<consumed_energy description="Energy amount">
<value>7202057977</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</taxi_out_energy>
<taxi_in_energy ID="0" description="Amount of energy needed for taxiing at destination for specified energy carrier">
<consumed_energy description="Energy amount">
<value>4001143321</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1e+13</upper_boundary>
</consumed_energy>
<energy_carrier_ID description="See energy carrier specification node">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5</upper_boundary>
</energy_carrier_ID>
</taxi_in_energy>
</taxi_energy>
<block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
<value>7856.162369</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>45000</upper_boundary>
</block_time>
<flight_time description="Flight time for the whole mission">
<value>7016.162369</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>44500</upper_boundary>
</flight_time>
<takeoff_engine_derate description="Engine power demand">
<value>1</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</takeoff_engine_derate>
<cruise description="Characteristics of the cruise segment">
<average_lift_coefficient description="Lift coefficient CL_average: Arithmetic mean over the entire cruise flight">
<value>0.4761674741</value>
<unit>1</unit>
<lower_boundary>-0.01</lower_boundary>
<upper_boundary>1</upper_boundary>
</average_lift_coefficient>
<minimum_lift_coefficient description="Minimum cruise flight lift coefficient CL_min">
<value>0.4728031554</value>
<unit>1</unit>
<lower_boundary>-0.01</lower_boundary>
<upper_boundary>1</upper_boundary>
</minimum_lift_coefficient>
<maximum_lift_coefficient description="Maximum cruise flight lift coefficient CL_max">
<value>0.5048791966</value>
<unit>1</unit>
<lower_boundary>-0.01</lower_boundary>
<upper_boundary>1</upper_boundary>
</maximum_lift_coefficient>
<top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
<value>66532.93487</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>150000</upper_boundary>
</top_of_climb_mass>
<top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
<value>65612.81266</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>150000</upper_boundary>
</top_of_descent_mass>
<top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
<value>194351.2576</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>4537400</upper_boundary>
</top_of_climb_range>
<top_of_descent_range description="Flown range from takeoff to top of descent">
<value>1272978.151</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>4537400</upper_boundary>
</top_of_descent_range>
<cruise_steps description="Cruise step information">
<cruise_step ID="0" description="Data of a cruise step">
<relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
<value>1</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</relative_end_of_cruise_step>
<altitude description="Altitude of cruise step">
<value>10668.00002</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>15000</upper_boundary>
</altitude>
</cruise_step>
</cruise_steps>
</cruise>
</study_mission>
</mission>
</analysis>
<component_design>
<global_reference_point>
<reference_component description="Global reference point of aircraft geometry">
<value>fuselage</value>
</reference_component>
<x description="X coordinate of the global reference point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</x>
<y description="Y coordinate of the global reference point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</y>
<z description="Z coordinate of the global reference point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</z>
</global_reference_point>
<wing>
<mass_properties description="mass_properties of component wing">
<mass description="component mass">
<value>7896.746484</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="component inertia referred to local center of gravity">
<j_xx description="wing inertia in x">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="wing inertia in y">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="wing inertia in z">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="wing inertia in xy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="wing inertia in xz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="wing inertia in yx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="wing inertia in yz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="wing inertia in zx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="wing inertia in zy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="component center of gravity with respect to global coordinate system">
<x description="x position of center of gravity">
<value>21.92220256</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</x>
<y description="y position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</y>
<z description="z position of center of gravity">
<value>-0.7035726591</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<position description="position of wing">
<x description="x position">
<value>17.75145044</value>
<unit>1</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</x>
<y description="y position">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z position">
<value>-1.030571436</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<specific>
<geometry>
<aerodynamic_surface ID="0" description="main_wing">
<name description="name of surface">
<value>main_wing</value>
</name>
<position description="reference position in aircraft coordinates">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<parameters description="aerodynamic surface parameters">
<direction description="unit vector according to aircraft coordinate system for direction applied at position">
<x description="x direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y direction of unit vector">
<value>-1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</direction>
<symmetric description="symmetric to local x-z plane">
<value>true</value>
</symmetric>
<sections description="sections">
<section ID="0">
<chord_origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</chord_origin>
<chord_length description="chord length of the section">
<value>6.458219551</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<scale_thickness description="scale the thickness defined by the profile with this factor">
<value>1.00040016</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</scale_thickness>
<profile description="profile (data normalized to chord length)">
<value>F15_15</value>
</profile>
</section>
<section ID="1">
<chord_origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-1.983993414</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</chord_origin>
<chord_length description="chord length of the section">
<value>6.458219551</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<scale_thickness description="scale the thickness defined by the profile with this factor">
<value>1.00040016</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</scale_thickness>
<profile description="profile (data normalized to chord length)">
<value>F15_15</value>
</profile>
</section>
<section ID="2">
<chord_origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>2.035403072</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0.2355374897</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-5.352336445</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</chord_origin>
<chord_length description="chord length of the section">
<value>4.599343857</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<scale_thickness description="scale the thickness defined by the profile with this factor">
<value>0.9209974332</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</scale_thickness>
<profile description="profile (data normalized to chord length)">
<value>F15_15</value>
</profile>
</section>
<section ID="3">
<chord_origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>8.734380802</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>1.108838412</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-17.84112148</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</chord_origin>
<chord_length description="chord length of the section">
<value>1.097897324</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<scale_thickness description="scale the thickness defined by the profile with this factor">
<value>0.6265964242</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</scale_thickness>
<profile description="profile (data normalized to chord length)">
<value>F15_15</value>
</profile>
</section>
</sections>
<spars>
<spar ID="0" description="front_spar">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
</spar>
<spar ID="1" description="rear_spar">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
</spar>
</spars>
<control_devices>
<control_device ID="0" description="slat">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.1134274706</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.294</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.6981317008</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
<control_device ID="1" description="slat">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.306</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.95</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.6981317008</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
<control_device ID="2" description="flap_fowler">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.75</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.1134274706</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.75</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.297</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.7853981634</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
<control_device ID="3" description="flap_fowler">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.75</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.303</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.75</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.78</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.7853981634</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
<control_device ID="4" description="aileron">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.8</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.98</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>-0.3490658504</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.3490658504</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
<control_device ID="5" description="spoiler_ground">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.2037137353</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.294</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.7853981634</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
<control_device ID="6" description="spoiler_air">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.306</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.4195</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.7853981634</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
<control_device ID="7" description="spoiler_air">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.4195</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.533</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.7853981634</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
<control_device ID="8" description="spoiler_air">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.533</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.6465</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.7853981634</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
<control_device ID="9" description="spoiler_air">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.6465</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.85</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.76</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.7853981634</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
</control_devices>
</parameters>
</aerodynamic_surface>
</geometry>
</specific>
</wing>
<empennage>
<position description="position of empennage">
<x description="x position">
<value>41.19599159</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y position">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z position">
<value>0.92429206</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<mass_properties description="mass_properties of component Conventional tail overall mass">
<mass description="component mass">
<value>983.6646752</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="component inertia referred to local center of gravity">
<j_xx description="Conventional tail overall mass inertia in x">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="Conventional tail overall mass inertia in y">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="Conventional tail overall mass inertia in z">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="Conventional tail overall mass inertia in xy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="Conventional tail overall mass inertia in xz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="Conventional tail overall mass inertia in yx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="Conventional tail overall mass inertia in yz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="Conventional tail overall mass inertia in zx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="Conventional tail overall mass inertia in zy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="component center of gravity with respect to global coordinate system">
<x description="x position of center of gravity">
<value>45.24364245</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</x>
<y description="y position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</y>
<z description="z position of center of gravity">
<value>3.000638678</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<specific>
<geometry>
<aerodynamic_surface ID="0" description="vertical_stabiliser">
<name description="name of surface">
<value>vertical_stabiliser</value>
</name>
<position description="reference position in aircraft coordinates">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<parameters description="aerodynamic surface parameters">
<direction description="unit vector according to aircraft coordinate system for direction applied at position">
<x description="x direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z direction of unit vector">
<value>-1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</direction>
<symmetric description="symmetric to local x-z plane">
<value>false</value>
</symmetric>
<sections description="sections">
<section ID="0">
<chord_origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</chord_origin>
<chord_length description="chord length of the section">
<value>5.31423154</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<scale_thickness description="scale the thickness defined by the profile with this factor">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</scale_thickness>
<profile description="profile (data normalized to chord length)">
<value>n0012</value>
</profile>
</section>
<section ID="1">
<chord_origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>4.81324168</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-6.387387456</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</chord_origin>
<chord_length description="chord length of the section">
<value>1.409334205</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<scale_thickness description="scale the thickness defined by the profile with this factor">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</scale_thickness>
<profile description="profile (data normalized to chord length)">
<value>n0012</value>
</profile>
</section>
</sections>
<spars>
<spar ID="0" description="front_spar">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
</spar>
<spar ID="1" description="rear_spar">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
</spar>
</spars>
<control_devices>
<control_device ID="0" description="rudder">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.9</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>-0.4363323125</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.4363323125</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
</control_devices>
</parameters>
<mass_properties description="mass_properties of component vertical stabiliser mass">
<mass description="component mass">
<value>417.1115867</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</mass>
<inertia description="component inertia referred to local center of gravity">
<j_xx description="vertical stabiliser mass inertia in x">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="vertical stabiliser mass inertia in y">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="vertical stabiliser mass inertia in z">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="vertical stabiliser mass inertia in xy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="vertical stabiliser mass inertia in xz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="vertical stabiliser mass inertia in yx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="vertical stabiliser mass inertia in yz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="vertical stabiliser mass inertia in zx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="vertical stabiliser mass inertia in zy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="component center of gravity with respect to global coordinate system">
<x description="x position of center of gravity">
<value>44.44562535</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z position of center of gravity">
<value>3.499710377</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
</aerodynamic_surface>
<aerodynamic_surface ID="1" description="horizontal_stabiliser">
<name description="name of surface">
<value>horizontal_stabiliser</value>
</name>
<position description="reference position in aircraft coordinates">
<x description="x coordinate of point">
<value>2.3164928</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-0.5869856587</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<parameters description="aerodynamic surface parameters">
<direction description="unit vector according to aircraft coordinate system for direction applied at position">
<x description="x direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y direction of unit vector">
<value>-1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</direction>
<symmetric description="symmetric to local x-z plane">
<value>true</value>
</symmetric>
<sections description="sections">
<section ID="0">
<chord_origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</chord_origin>
<chord_length description="chord length of the section">
<value>3.497738739</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<scale_thickness description="scale the thickness defined by the profile with this factor">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</scale_thickness>
<profile description="profile (data normalized to chord length)">
<value>n0012</value>
</profile>
</section>
<section ID="1">
<chord_origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>3.259282429</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0.3947538294</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-5.645242769</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</chord_origin>
<chord_length description="chord length of the section">
<value>0.9870618726</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<scale_thickness description="scale the thickness defined by the profile with this factor">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</scale_thickness>
<profile description="profile (data normalized to chord length)">
<value>n0012</value>
</profile>
</section>
</sections>
<spars>
<spar ID="0" description="front_spar">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
</spar>
<spar ID="1" description="rear_spar">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>0.6</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
</spar>
</spars>
<control_devices>
<control_device ID="0" description="elevator">
<position description="relative chord position">
<inner_position description="relative inner position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.2</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</inner_position>
<outer_position description="relative outer position">
<chord description="chord position">
<from description="relative chord position">
<value>0.7</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</from>
<to description="relative chord position">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</to>
</chord>
<spanwise description="relative spanwise position">
<value>-0.9</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</spanwise>
</outer_position>
</position>
<deflection>
<full_negative_deflection description="full negative deflection">
<value>-0.4363323125</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_negative_deflection>
<full_positive_deflection description="full positive deflection">
<value>0.4363323125</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</full_positive_deflection>
</deflection>
</control_device>
</control_devices>
</parameters>
<mass_properties description="mass_properties of component horizontal stabiliser mass">
<mass description="component mass">
<value>566.5530885</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</mass>
<inertia description="component inertia referred to local center of gravity">
<j_xx description="horizontal stabiliser mass inertia in x">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="horizontal stabiliser mass inertia in y">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="horizontal stabiliser mass inertia in z">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="horizontal stabiliser mass inertia in xy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="horizontal stabiliser mass inertia in xz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="horizontal stabiliser mass inertia in yx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="horizontal stabiliser mass inertia in yz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="horizontal stabiliser mass inertia in zx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="horizontal stabiliser mass inertia in zy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="component center of gravity with respect to global coordinate system">
<x description="x position of center of gravity">
<value>45.83116405</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z position of center of gravity">
<value>2.633208702</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
</aerodynamic_surface>
</geometry>
</specific>
</empennage>
<propulsion>
<position description="Reference position of the propulsion assembly">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of the propulsion assembly">
<mass description="mass of the of the component">
<value>9147.202805</value>
<unit>kg</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of the component in respect to the CG">
<j_xx description="inertia of the component">
<value>357715.0023</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="inertia of the component">
<value>15621.01016</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="inertia of the component">
<value>364726.4249</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="inertia of the component">
<value>-0.06634606414</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="inertia of the component">
<value>3560.102271</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="inertia of the component">
<value>-0.06634606414</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="inertia of the component">
<value>-0.009678976632</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="inertia of the component">
<value>3560.102271</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="inertia of the component">
<value>-0.009678976632</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
<x description="x coordinate of the center of gravity">
<value>18.31595065</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of the center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of the center of gravity">
<value>-2.356641711</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<specific>
<propulsion ID="0" description="Description of one propulsion">
<nacelle ID="0" description="Nacelle of the propulsion assembly">
<position description="Origin of the nacelle RELATIVE to the engine position.">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<normal description="Normal direction of the nacelle in the global aircraft coordinate system">
<x description="x direction of unit vector">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</normal>
<sections description="Geometrical description nacelle sections">
<section ID="0">
<origin description="Origin of the section (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<width description="width of the section">
<value>2.261851375</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</width>
<height description="Height of the section">
<value>2.261851375</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</height>
<profile description="The profile name of the section">
<value>nacelle</value>
</profile>
</section>
<section ID="1">
<origin description="Origin of the section (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0.8618070959</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<width description="width of the section">
<value>2.736840163</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</width>
<height description="Height of the section">
<value>2.736840163</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</height>
<profile description="The profile name of the section">
<value>nacelle</value>
</profile>
</section>
<section ID="2">
<origin description="Origin of the section (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>2.585421288</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<width description="width of the section">
<value>2.736840163</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</width>
<height description="Height of the section">
<value>2.736840163</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</height>
<profile description="The profile name of the section">
<value>nacelle</value>
</profile>
</section>
<section ID="3">
<origin description="Origin of the section (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>3.447228384</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<width description="width of the section">
<value>2.261851375</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</width>
<height description="Height of the section">
<value>2.261851375</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</height>
<profile description="The profile name of the section">
<value>nacelle</value>
</profile>
</section>
</sections>
<mass_properties description="Mass properties of the nacelle">
<mass description="mass of the of the component">
<value>1077.525351</value>
<unit>kg</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</mass>
<inertia description="Inertia of the component in respect to the CG">
<j_xx description="inertia of the component">
<value>49.05540588</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="inertia of the component">
<value>51.64642853</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="inertia of the component">
<value>51.6456818</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="inertia of the component">
<value>-0.002397325367</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="inertia of the component">
<value>0.006676311088</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="inertia of the component">
<value>-0.002397325367</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="inertia of the component">
<value>-0.002390716634</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="inertia of the component">
<value>0.006676311088</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="inertia of the component">
<value>-0.002390716634</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
<x description="x coordinate of the center of gravity">
<value>18.03856294</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of the center of gravity">
<value>-6.198639603</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of the center of gravity">
<value>-2.540481562</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
</nacelle>
<pylon ID="0" description="pylon of the propulsion assembly">
<position description="Position of the pylon RELATIVE to the engine position.">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<normal description="unit vector according to aircraft coordinate system for direction applied at position">
<x description="x direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z direction of unit vector">
<value>-1.130925687</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</normal>
<sections description="sections">
<section ID="0">
<origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>0.8618070959</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>1.675831273e-16</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-1.368420082</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<chord_length description="chord length of the section">
<value>3.447228384</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<profile description="profile (data normalized to chord length)">
<value>pylon</value>
</profile>
</section>
<section ID="1">
<origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>3.925861338</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>2.210030553e-16</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-1.804626897</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<chord_length description="chord length of the section">
<value>3.447228384</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<profile description="profile (data normalized to chord length)">
<value>pylon</value>
</profile>
</section>
</sections>
<mass_properties description="Mass properties of the pylon">
<mass description="mass of the of the component">
<value>529.9702159</value>
<unit>kg</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of the component in respect to the CG">
<j_xx description="inertia of the component">
<value>0.1461895291</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="inertia of the component">
<value>8.726965415</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="inertia of the component">
<value>8.731134911</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="inertia of the component">
<value>-0.0307757067</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="inertia of the component">
<value>0.5146596874</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="inertia of the component">
<value>-0.0307757067</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="inertia of the component">
<value>-0.002448771663</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="inertia of the component">
<value>0.5146596874</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="inertia of the component">
<value>-0.002448771663</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
<x description="x coordinate of the center of gravity">
<value>20.43239715</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</x>
<y description="y coordinate of the center of gravity">
<value>-6.198639603</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</y>
<z description="z coordinate of the center of gravity">
<value>-0.9539580722</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
</pylon>
<engine>
<model description="Name of selected engine model">
<value>PW1127G-JM-H2</value>
</model>
<position description="Position of the engine in the global coordinate system">
<x description="x coordinate of point">
<value>16.31494874</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>-6.198639603</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-2.540481562</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of the engine">
<mass description="mass of the of the component">
<value>2966.105836</value>
<unit>kg</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of the component in respect to the CG">
<j_xx description="inertia of the component">
<value>1896.814168</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="inertia of the component">
<value>3885.688187</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="inertia of the component">
<value>3885.688187</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
<x description="x coordinate of the center of gravity">
<value>18.03856294</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</x>
<y description="y coordinate of the center of gravity">
<value>-6.198639603</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</y>
<z description="z coordinate of the center of gravity">
<value>-2.540481562</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<SLST description="Sea level static thrust of the engine">
<value>123616.7566</value>
<unit>N</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</SLST>
<scale_factor description="Scale factor of the engine">
<value>1.03432867</value>
<unit>1</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</scale_factor>
<bucket_point description="Bucket point of the engine at initial cruise flight phase">
<thrust description="Thrust of the engine at the bucket point">
<value>21693.35253</value>
<unit>N</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</thrust>
<tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
<value>5.45681508e-06</value>
<unit>kg/Ns</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</tsfc>
</bucket_point>
</engine>
</propulsion>
<propulsion ID="1" description="Description of one propulsion">
<nacelle ID="0" description="Nacelle of the propulsion assembly">
<position description="Origin of the nacelle RELATIVE to the engine position.">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<normal description="Normal direction of the nacelle in the global aircraft coordinate system">
<x description="x direction of unit vector">
<value>1</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</normal>
<sections description="Geometrical description nacelle sections">
<section ID="0">
<origin description="Origin of the section (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<width description="width of the section">
<value>2.261851375</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</width>
<height description="Height of the section">
<value>2.261851375</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</height>
<profile description="The profile name of the section">
<value>nacelle</value>
</profile>
</section>
<section ID="1">
<origin description="Origin of the section (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0.8618070959</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<width description="width of the section">
<value>2.736840163</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</width>
<height description="Height of the section">
<value>2.736840163</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</height>
<profile description="The profile name of the section">
<value>nacelle</value>
</profile>
</section>
<section ID="2">
<origin description="Origin of the section (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>2.585421288</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<width description="width of the section">
<value>2.736840163</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</width>
<height description="Height of the section">
<value>2.736840163</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</height>
<profile description="The profile name of the section">
<value>nacelle</value>
</profile>
</section>
<section ID="3">
<origin description="Origin of the section (local)">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>3.447228384</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<width description="width of the section">
<value>2.261851375</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</width>
<height description="Height of the section">
<value>2.261851375</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</height>
<profile description="The profile name of the section">
<value>nacelle</value>
</profile>
</section>
</sections>
<mass_properties description="Mass properties of the nacelle">
<mass description="mass of the of the component">
<value>1077.525351</value>
<unit>kg</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</mass>
<inertia description="Inertia of the component in respect to the CG">
<j_xx description="inertia of the component">
<value>49.05540588</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="inertia of the component">
<value>51.64642853</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="inertia of the component">
<value>51.6456818</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="inertia of the component">
<value>-0.002397325367</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="inertia of the component">
<value>0.006676311088</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="inertia of the component">
<value>-0.002397325367</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="inertia of the component">
<value>-0.002390716634</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="inertia of the component">
<value>0.006676311088</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="inertia of the component">
<value>-0.002390716634</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
<x description="x coordinate of the center of gravity">
<value>18.03856294</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of the center of gravity">
<value>6.198639603</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of the center of gravity">
<value>-2.540481562</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
</nacelle>
<pylon ID="0" description="pylon of the propulsion assembly">
<position description="Position of the pylon RELATIVE to the engine position.">
<x description="x coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<normal description="unit vector according to aircraft coordinate system for direction applied at position">
<x description="x direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y direction of unit vector">
<value>0</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z direction of unit vector">
<value>-1.130925687</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</normal>
<sections description="sections">
<section ID="0">
<origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>0.8618070959</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>1.675831273e-16</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-1.368420082</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<chord_length description="chord length of the section">
<value>3.447228384</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<profile description="profile (data normalized to chord length)">
<value>pylon</value>
</profile>
</section>
<section ID="1">
<origin description="origin of chord (local)">
<x description="x coordinate of point">
<value>3.925861338</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>2.210030553e-16</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-1.804626897</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</origin>
<chord_length description="chord length of the section">
<value>3.447228384</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</chord_length>
<geometric_twist description="geometric twist of the section around leading edge">
<value>-0</value>
<unit>rad</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</geometric_twist>
<profile description="profile (data normalized to chord length)">
<value>pylon</value>
</profile>
</section>
</sections>
<mass_properties description="Mass properties of the pylon">
<mass description="mass of the of the component">
<value>529.9702159</value>
<unit>kg</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of the component in respect to the CG">
<j_xx description="inertia of the component">
<value>0.1461895291</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="inertia of the component">
<value>8.726965415</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="inertia of the component">
<value>8.731134911</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="inertia of the component">
<value>-0.0307757067</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="inertia of the component">
<value>0.5146596874</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="inertia of the component">
<value>-0.0307757067</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="inertia of the component">
<value>-0.002448771663</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="inertia of the component">
<value>0.5146596874</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="inertia of the component">
<value>-0.002448771663</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
<x description="x coordinate of the center of gravity">
<value>20.43239715</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</x>
<y description="y coordinate of the center of gravity">
<value>6.198639603</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</y>
<z description="z coordinate of the center of gravity">
<value>-0.9539580722</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
</pylon>
<engine>
<model description="Name of selected engine model">
<value>PW1127G-JM-H2</value>
</model>
<position description="Position of the engine in the global coordinate system">
<x description="x coordinate of point">
<value>16.31494874</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y coordinate of point">
<value>6.198639603</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z coordinate of point">
<value>-2.540481562</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of the engine">
<mass description="mass of the of the component">
<value>2966.105836</value>
<unit>kg</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of the component in respect to the CG">
<j_xx description="inertia of the component">
<value>1896.814168</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="inertia of the component">
<value>3885.688187</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="inertia of the component">
<value>3885.688187</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="inertia of the component">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
<x description="x coordinate of the center of gravity">
<value>18.03856294</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</x>
<y description="y coordinate of the center of gravity">
<value>6.198639603</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</y>
<z description="z coordinate of the center of gravity">
<value>-2.540481562</value>
<unit>m</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<SLST description="Sea level static thrust of the engine">
<value>123616.7566</value>
<unit>N</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</SLST>
<scale_factor description="Scale factor of the engine">
<value>1.03432867</value>
<unit>1</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</scale_factor>
<bucket_point description="Bucket point of the engine at initial cruise flight phase">
<thrust description="Thrust of the engine at the bucket point">
<value>21693.35253</value>
<unit>N</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</thrust>
<tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
<value>5.45681508e-06</value>
<unit>kg/Ns</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</tsfc>
</bucket_point>
</engine>
</propulsion>
</specific>
</propulsion>
<systems>
<mass_properties description="mass_properties of component systems">
<mass description="component mass">
<value>6615.723065</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</mass>
<inertia description="component inertia referred to local center of gravity">
<j_xx description="systems inertia in x">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="systems inertia in y">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="systems inertia in z">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="systems inertia in xy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="systems inertia in xz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="systems inertia in yx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="systems inertia in yz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="systems inertia in zx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="systems inertia in zy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="component center of gravity with respect to global coordinate system">
<x description="x position of center of gravity">
<value>10.49455393</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<operator_items>
<operator_item ID="0">
<name description="name of the operator item">
<value>water_and_toilet_chemicals</value>
</name>
<mass_properties description="mass_properties of component water and toilet chemicals">
<mass description="component mass">
<value>244.8</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</mass>
<inertia description="component inertia referred to local center of gravity">
<j_xx description="water and toilet chemicals inertia in x">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="water and toilet chemicals inertia in y">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="water and toilet chemicals inertia in z">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="water and toilet chemicals inertia in xy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="water and toilet chemicals inertia in xz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="water and toilet chemicals inertia in yx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="water and toilet chemicals inertia in yz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="water and toilet chemicals inertia in zx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="water and toilet chemicals inertia in zy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="component center of gravity with respect to global coordinate system">
<x description="x position of center of gravity">
<value>3.229109776</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
</operator_item>
<operator_item ID="1">
<name description="name of the operator item">
<value>residual_oil_and_fuel</value>
</name>
<mass_properties description="mass_properties of component water and toilet chemicals">
<mass description="component mass">
<value>2.799540704</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</mass>
<inertia description="component inertia referred to local center of gravity">
<j_xx description="water and toilet chemicals inertia in x">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xx>
<j_yy description="water and toilet chemicals inertia in y">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yy>
<j_zz description="water and toilet chemicals inertia in z">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zz>
<j_xy description="water and toilet chemicals inertia in xy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xy>
<j_xz description="water and toilet chemicals inertia in xz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_xz>
<j_yx description="water and toilet chemicals inertia in yx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yx>
<j_yz description="water and toilet chemicals inertia in yz">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_yz>
<j_zx description="water and toilet chemicals inertia in zx">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zx>
<j_zy description="water and toilet chemicals inertia in zy">
<value>0</value>
<unit>kgm^2</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="component center of gravity with respect to global coordinate system">
<x description="x position of center of gravity">
<value>21.92220256</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</x>
<y description="y position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</y>
<z description="z position of center of gravity">
<value>0</value>
<unit>m</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
</operator_item>
</operator_items>
<specific>
<geometry>
<mass_properties>
<fuel_system description="mass of ATA-28">
<value>476.7269182</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</fuel_system>
<de_icing description="mass of ATA-30">
<value>50.0353201</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</de_icing>
<lighting description="mass of ATA-33">
<value>255.9890824</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</lighting>
<fire_protection description="mass of ATA-26">
<value>89.90290824</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</fire_protection>
<oxygen_system description="mass of ATA-35">
<value>114.784</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</oxygen_system>
<flight_controls description="mass of ATA-27">
<value>706.182169</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</flight_controls>
<instruments description="mass of ATA31">
<value>93.41552608</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</instruments>
<automatic_flight_system description="mass of ATA22">
<value>151.8002299</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</automatic_flight_system>
<navigation description="mass of ATA34">
<value>618.8778603</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</navigation>
<communication description="mass of ATA23">
<value>303.6004598</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</communication>
<bleed_air_system description="mass of ATA-36">
<value>219.7746979</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</bleed_air_system>
<hydraulic_generation description="mass of ATA-29">
<value>178.2241792</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</hydraulic_generation>
<hydraulic_distribution description="mass of ATA-29">
<value>715.1778549</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</hydraulic_distribution>
<electrical_generation description="mass of ATA-24">
<value>763.2564568</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</electrical_generation>
<electrical_distribution description="mass of ATA-24">
<value>645.1221143</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</electrical_distribution>
<auxiliary_power_unit description="mass of ATA-49">
<value>220.4595807</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</auxiliary_power_unit>
<air_conditioning description="mass of ATA-21">
<value>764.7941666</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</air_conditioning>
</mass_properties>
</geometry>
<maximium_power_demand description="maximum power (hydraulic + electric) demand">
<value>372179.1673</value>
<unit>W</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</maximium_power_demand>
<maximium_bleed_air_demand description="maximum bleed air demand">
<value>2.397104381</value>
<unit>kg/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</maximium_bleed_air_demand>
<average_power_demand description="average power (hydraulic + electric) demand">
<value>125700.3236</value>
<unit>W</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</average_power_demand>
<average_bleed_air_demand description="average bleed air demand">
<value>1.024591634</value>
<unit>kg/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100</upper_boundary>
</average_bleed_air_demand>
</specific>
</systems>
<fuselage description="Geometric description of the aircraft fuselage." tool_level="1">
<position description="Position of the fuselages with regard to the global reference point.">
<x description="Distance in x direction with regard to the global reference point. (fuselage nose point)">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point. (fuselage nose point)">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-25</lower_boundary>
<upper_boundary>25</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point. (fuselage nose point)">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of all fuselages.">
<mass description="Mass of all fuselages.">
<value>22532.25982</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of all fuselages with regard to the total center of gravity.">
<j_xx description="Inertia of the of all fuselages in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia of the of all fuselages in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia of the of all fuselages in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia of all fuselages in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia of all fuselages in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia of all fuselages in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia of all fuselages in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia of all fuselages in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia of all fuselages in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of all fuselages.">
<x description="Center of gravity in x-direction with regard to the global reference point. (of all fuselages)">
<value>21.6379044</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>50</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point. (of all fuselages)">
<value>0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point. (of all fuselages)">
<value>-0.2413</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<specific description="Fuselage design specific output parameter.">
<geometry description="Geometry description of the entire fuselage design.">
<fuselage ID="0" description="Geometrical description of one entire fuselage.">
<name description="Name of the fuselage.">
<value>fuselage_0</value>
</name>
<position description="Position of one entire fuselage with regard to the fuselage global position.">
<x description="Distance in x direction with regard to the fuselage gear global position.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Distance in y direction with regard to the fuselage gear global position.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-25</lower_boundary>
<upper_boundary>25</upper_boundary>
</y>
<z description="Distance in z direction with regard to the fuselage gear global position.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</position>
<direction description="Unit vector according to global coordinate system for direction applied at position.">
<x description="X component of the unit vector.">
<value>1</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</x>
<y description="Y component of the unit vector.">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</y>
<z description="Z component of the unit vector.">
<value>0</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</z>
</direction>
<mass_properties description="Mass properties of one entire fuselage.">
<mass description="Mass of one entire fuselage.">
<value>22532.259823558</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
<inertia description="Inertia of one entire fuselage with regard to his center of gravity.">
<j_xx description="Inertia of one entire fuselage in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia of one entire fuselage in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia of one entire fuselage in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia of one entire fuselage in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia of one entire fuselage in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia of one entire fuselage in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia of one entire fuselage in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia of one entire fuselage in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia of one entire fuselage in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of one entire fuselage.">
<x description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>50</upper_boundary>
</x>
<y description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-25</lower_boundary>
<upper_boundary>25</upper_boundary>
</y>
<z description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<sections description="Geometrical description of the fuselage sections of one entire fuselage.">
<section ID="0" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_0</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.957580772</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>0.068075648</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>0.236859405</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>0.267845269</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>0.496500597</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="1" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_1</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.924669034</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>0.192850112</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>0.410780143</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>0.467251904</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>0.836740921</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="2" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_2</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.88671607</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>0.325974005</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>0.51432337</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>0.617142191</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>1.09949371</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="3" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_3</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.814819481</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>0.552671561</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>0.638938798</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>0.811819183</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>1.332869486</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="4" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_4</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.746964181</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>0.779068819</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>0.756396515</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>0.976541153</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>1.597847703</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="5" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_5</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.624593025</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>1.123655542</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>0.945319536</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>1.211739628</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>1.950706682</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="6" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_6</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.499674101</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>1.438280013</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.097107435</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>1.430154001</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>2.243644807</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="7" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_7</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.21769763</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>2.128158942</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.34967515</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>1.867790838</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>2.796234326</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="8" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_8</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.174885536</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>2.619107088</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.558414858</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>1.972433715</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.095828445</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="9" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_9</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.083279283</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>3.445878719</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.734079899</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>2.114075921</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.508608277</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="10" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_10</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>-0.041639641</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>4.194982413</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.833938046</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>2.167619711</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.762303773</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="11" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_11</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>5.168818078</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.877197398</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>2.219703367</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.908262138</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="12" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_12</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>6.2175644</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.915417119</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>2.227583628</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.967986828</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="13" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_13</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>6.2175644</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.915417119</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>2.227583628</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.967986828</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="14" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_14</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>38.14663462</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.915413925</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>2.227579912</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.967986828</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="15" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_15</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>38.14663462</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.915413925</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>2.227579912</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.967986828</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="16" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_16</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>42.57228328</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.699062858</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>1.736999316</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.3288491</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="17" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_17</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>43.42065009</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.657090968</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>1.517589228</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>3.095828445</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="18" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_18</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>45.11738369</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>1.575335554</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>0.93980933</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>2.46334671</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
<section ID="19" description="Geometrical description of one fuselage section.">
<name description="Name of the fuselage section.">
<value>section_19</value>
</name>
<section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
<value>ellipse</value>
</section_shape>
<origin description="Origin of fuselage section (local).">
<x description="Distance in x direction with regard to the global reference point.">
<value>-0</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point.">
<value>0.92429206</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point.">
<value>48.07829878</value>
<unit>m</unit>
<lower_boundary>-75</lower_boundary>
<upper_boundary>75</upper_boundary>
</z>
</origin>
<upper_height description="Height of the upper half of the fuselage section.">
<value>0.528165979</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</upper_height>
<lower_height description="Height of the lower half of the fuselage section.">
<value>0.614244216</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</lower_height>
<width description="Width of the fuselage section.">
<value>0.559150813</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</width>
</section>
</sections>
<number_of_required_cabin_crew description="Number of minimum required flight attendants.">
<value>4</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100</upper_boundary>
</number_of_required_cabin_crew>
<number_of_required_flight_crew description="Number of minimum required flight crew members.">
<value>2</value>
<unit>1</unit>
<lower_boundary>1</lower_boundary>
<upper_boundary>4</upper_boundary>
</number_of_required_flight_crew>
<mass_breakdown description="Mass breakdown of fuselage design module in accordance to CPACS.">
<fuselage_structure description="Mass breakdown of the fuselage structure block.">
<component_mass ID="0" description="Mass of a single component of the fuselage structure block.">
<name description="Name of the fuselage structure component.">
<value>door_mass</value>
</name>
<mass description="Mass of the fuselage structure component.">
<value>360.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="1" description="Mass of a single component of the fuselage structure block.">
<name description="Name of the fuselage structure component.">
<value>fuselage_mass</value>
</name>
<mass description="Mass of the fuselage structure component.">
<value>14716.991711297</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
</fuselage_structure>
<fuselage_furnishing description="Mass breakdown of the fuselage furnishing block.">
<component_mass ID="0" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>lavatory_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>290.01</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="1" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>flight_attendant_seat_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>48.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="2" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>floor_covering_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>159.641751426</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="3" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>wall_covering_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>289.30950138</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="4" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>ceiling_covering_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>106.98516576</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="5" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>linings_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>396.29466714</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="6" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>acoustic_and_thermal_insolation_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>619.575445338</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="7" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>overhead_bin_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>351.213928</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="8" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>passenger_safety_unit_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>90.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="9" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>lightning_panel_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>72.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="10" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>oxygen_system_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>201.51999999999998</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="11" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>cargo_linings_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>431.346961788</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="12" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>cargo_loadings_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>672.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="13" description="Mass of a single component of the fuselage furnishing block.">
<name description="Name of the fuselage furnishing component.">
<value>miscellaneous_mass</value>
</name>
<mass description="Mass of the fuselage furnishing component.">
<value>324.160275369</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
</fuselage_furnishing>
<fuselage_operator_items description="Mass breakdown of the fuselage operator items block.">
<component_mass ID="0" description="Mass of a single component of the fuselage operator items block.">
<name description="Name of the fuselage operator items component.">
<value>total_emergency_equipment_masses</value>
</name>
<mass description="Mass of the fuselage operator item component.">
<value>840.4850832</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="1" description="Mass of a single component of the fuselage operator items block.">
<name description="Name of the fuselage operator items component.">
<value>flight_attendant_mass</value>
</name>
<mass description="Mass of the fuselage operator item component.">
<value>280.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="2" description="Mass of a single component of the fuselage operator items block.">
<name description="Name of the fuselage operator items component.">
<value>flight_crew_mass</value>
</name>
<mass description="Mass of the fuselage operator item component.">
<value>170.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="3" description="Mass of a single component of the fuselage operator items block.">
<name description="Name of the fuselage operator items component.">
<value>in_flight_entertainment</value>
</name>
<mass description="Mass of the fuselage operator item component.">
<value>90.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="4" description="Mass of a single component of the fuselage operator items block.">
<name description="Name of the fuselage operator items component.">
<value>total_fixed_galley_mass</value>
</name>
<mass description="Mass of the fuselage operator item component.">
<value>315.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="5" description="Mass of a single component of the fuselage operator items block.">
<name description="Name of the fuselage operator items component.">
<value>total_seat_mass</value>
</name>
<mass description="Mass of the fuselage operator item component.">
<value>1242.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="6" description="Mass of a single component of the fuselage operator items block.">
<name description="Name of the fuselage operator items component.">
<value>catering_mass</value>
</name>
<mass description="Mass of the fuselage operator item component.">
<value>952.02</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
</fuselage_operator_items>
</mass_breakdown>
<fuselage_accommodation description="Description of the accommodation of current fuselage.">
<position description="Position of the payload tubes with regard to the fuselage position.">
<x description="Distance in x direction with regard to the fuselage position.">
<value>3.75</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Distance in y direction with regard to the fuselage position.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-0</lower_boundary>
<upper_boundary>0</upper_boundary>
</y>
<z description="Distance in z direction with regard to the fuselage position.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of the payload tubes of one entire fuselage.">
<mass description="Mass of the payload tubes of one entire fuselage.">
<value>7455.268112261</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
<center_of_gravity description="Center of gravity of all payload tubes.">
<x description="Center of gravity in x-direction with regard to the center of gravity of the fuselage.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>50</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the center of gravity of the fuselage.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the center of gravity of the fuselage.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<payload_tube ID="0" description="Geometrical description of one payload tube of the fuselage.">
<name description="Name of the payload tube.">
<value>center_payload_tube</value>
</name>
<payload_tube_reference_points description="Payload tube center reference points in x, y and z-direction referred to fuselage nose point.">
<front_reference_points description="Reference points in the front of payload tube.">
<x description="Payload tube reference point in x-direction.">
<value>0</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Payload tube reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>35</upper_boundary>
</y>
<z description="Payload tube reference point in z-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-15</lower_boundary>
<upper_boundary>15</upper_boundary>
</z>
<upper_z description="Upper payload tube reference point in z-direction.">
<value>1.778</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>15</upper_boundary>
</upper_z>
<lower_z description="Lower payload tube reference point in z-direction.">
<value>-2.090166</value>
<unit>m</unit>
<lower_boundary>-15</lower_boundary>
<upper_boundary>0</upper_boundary>
</lower_z>
</front_reference_points>
<aft_reference_points description="Reference points in the aft of payload tube.">
<x description="Payload tube reference point in x-direction.">
<value>27.016456</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Payload tube reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>35</upper_boundary>
</y>
<z description="Payload tube reference point in z-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-15</lower_boundary>
<upper_boundary>15</upper_boundary>
</z>
<upper_z description="Upper payload tube reference point in z-direction.">
<value>1.778</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>15</upper_boundary>
</upper_z>
<lower_z description="Lower payload tube reference point in z-direction.">
<value>-2.090166</value>
<unit>m</unit>
<lower_boundary>-15</lower_boundary>
<upper_boundary>0</upper_boundary>
</lower_z>
</aft_reference_points>
</payload_tube_reference_points>
<payload_tube_wall_reference_points description="Payload tube wall reference points in x, y and z-direction referred to fuselage nose point.">
<front_reference_points description="Reference points in the front of payload tube.">
<x description="Wall reference point in x-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<left_y description="Left wall reference point in y-direction.">
<value>-1.84658</value>
<unit>m</unit>
<lower_boundary>-35</lower_boundary>
<upper_boundary>35</upper_boundary>
</left_y>
<right_y description="Right wall reference point in y-direction.">
<value>1.84658</value>
<unit>m</unit>
<lower_boundary>-35</lower_boundary>
<upper_boundary>35</upper_boundary>
</right_y>
<z description="Wall reference point in z-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-15</lower_boundary>
<upper_boundary>15</upper_boundary>
</z>
</front_reference_points>
<aft_reference_points description="Reference points in the aft of payload tube.">
<x description="Wall reference point in x-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<left_y description="Left wall reference point in y-direction.">
<value>-1.84658</value>
<unit>m</unit>
<lower_boundary>-35</lower_boundary>
<upper_boundary>35</upper_boundary>
</left_y>
<right_y description="Right wall reference point in y-direction.">
<value>1.84658</value>
<unit>m</unit>
<lower_boundary>-35</lower_boundary>
<upper_boundary>35</upper_boundary>
</right_y>
<z description="Wall reference point in z-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-15</lower_boundary>
<upper_boundary>15</upper_boundary>
</z>
</aft_reference_points>
</payload_tube_wall_reference_points>
<payload_tube_structural_wall_thickness description="Structural wall thickness of the payload tube.">
<value>0.137414</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</payload_tube_structural_wall_thickness>
<payload_tube_water_volume description="Total water volume of one entire payload tube.">
<value>258.176893829</value>
<unit>m^3</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1000</upper_boundary>
</payload_tube_water_volume>
<payload_decks description="Geometrical description of the payload decks.">
<payload_deck ID="0" description="Geometrical description of the payload decks in one payload tube.">
<name description="Name of the payload deck.">
<value>passenger_deck_1</value>
</name>
<position description="Position of the payload deck with regard to the payload tube reference point.">
<x description="Distance in x direction with regard to the payload tube reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Distance in y direction with regard to the payload tube reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-0</lower_boundary>
<upper_boundary>0</upper_boundary>
</y>
<z description="Distance in z direction with regard to the payload tube reference point.">
<value>-0.4826</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</position>
<payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
<value>0.206248</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</payload_deck_structural_floor_thickness>
<payload_deck_water_volume description="Total water volume of the payload deck.">
<value>172.1179292</value>
<unit>m^3</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1000</upper_boundary>
</payload_deck_water_volume>
<payload_deck_length description="Total length of the payload deck.">
<value>27.016456</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100</upper_boundary>
</payload_deck_length>
<payload_deck_required_galley_power description="Required galley power of the payload deck.">
<value>9000</value>
<unit>W</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</payload_deck_required_galley_power>
</payload_deck>
<payload_deck ID="1" description="Geometrical description of the payload decks in one payload tube.">
<name description="Name of the payload deck.">
<value>cargo_deck</value>
</name>
<position description="Position of the payload deck with regard to the payload tube reference point.">
<x description="Distance in x direction with regard to the payload tube reference point.">
<value>3.75</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Distance in y direction with regard to the payload tube reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-0</lower_boundary>
<upper_boundary>0</upper_boundary>
</y>
<z description="Distance in z direction with regard to the payload tube reference point.">
<value>-1.831848</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</position>
<payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
<value>0.206248</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</payload_deck_structural_floor_thickness>
<payload_deck_water_volume description="Total water volume of the payload deck.">
<value>86.05896460966666</value>
<unit>m^3</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1000</upper_boundary>
</payload_deck_water_volume>
<payload_deck_length description="Total length of the payload deck.">
<value>13.508228</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100</upper_boundary>
</payload_deck_length>
<payload_deck_required_galley_power description="Required galley power of the payload deck.">
<value>0</value>
<unit>W</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</payload_deck_required_galley_power>
</payload_deck>
</payload_decks>
</payload_tube>
</fuselage_accommodation>
</fuselage>
</geometry>
</specific>
</fuselage>
<tank description="Description of aircraft tanks." tool_level="2">
<position description="Tank reference point, position of the tanks with regard to the global reference point.">
<x description="Distance between the foremost tank end and the global reference point in x-direction.">
<value>30.584919097564068</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the foremost tank end and the global reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</y>
<z description="Distance between the foremost middle tank end and the global reference point in z-direction.">
<value>-0.15608300249376805</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of all tanks.">
<mass description="Total tank mass.">
<value>2099.2609847846707</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of all tanks with regard to the total center of gravity.">
<j_xx description="Inertia of all tanks in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia of all tanks in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia of all tanks in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia of all tanks in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia of all tanks in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia of all tanks in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia of all tanks in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia of all tanks in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia of all tanks in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of all tanks.">
<x description="Center of gravity in x-direction with regard to the global reference point.">
<value>36.14497459013074</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-40</lower_boundary>
<upper_boundary>40</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point.">
<value>-0.09421024896405661</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<specific description="Tank design specific output parameter.">
<additional_fuselage_length description="Additional fuselage length (if smaller than 0: shrink fuselage, if greater than 0: stretch fuselage).">
<value>10.749603460904984</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>inf</upper_boundary>
</additional_fuselage_length>
<tank ID="0" description="Description of one tank.">
<name description="Name of the tank.">
<value>tank_0</value>
</name>
<designator description="Designator of the tank.">
<value>fuselage_tail_cone</value>
</designator>
<position description="Local reference point, position of one tank wrt. the tank reference point.">
<x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
<value>7.555080902</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-40</lower_boundary>
<upper_boundary>40</upper_boundary>
</y>
<z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
<value>0.027267186</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</position>
<direction description="Unit vector according to global coordinate system for direction applied at position.">
<x description="X component of the unit vector.">
<value>1</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</x>
<y description="Y component of the unit vector.">
<value>0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</y>
<z description="Z component of the unit vector.">
<value>0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</z>
</direction>
<mass_properties description="Mass properties of one tank.">
<mass description="Total dry mass of one tank.">
<value>721.0907415044228</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of one tank with regard to its center of gravity.">
<j_xx description="Inertia of the of one tank in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia of the of one tank in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia of the of one tank in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia of one tank in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia of one tank in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia of one tank in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia of one tank in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia of one tank in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia of one tank in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of one tank.">
<x description="Center of gravity in x-direction with regard to the local reference point.">
<value>1.6028937744784333</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the local reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-40</lower_boundary>
<upper_boundary>40</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the local reference point.">
<value>0.15285862860398236</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</center_of_gravity>
<centroid description="Centroid of one tank.">
<x description="Centroid in x-direction with regard to the local reference point.">
<value>1.602893774</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Centroid in y-direction with regard to the local reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-40</lower_boundary>
<upper_boundary>40</upper_boundary>
</y>
<z description="Centroid in z-direction with regard to the local reference point.">
<value>0.152858629</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</centroid>
</mass_properties>
<maximum_energy_capacity description="Maximum energy capacity of one tank.">
<value>1.621076599e+11</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</maximum_energy_capacity>
<energy_capacity_required_for_mission description="Energy amount required for mission.">
<value>true</value>
</energy_capacity_required_for_mission>
<geometry description="Geometrical description of one tank.">
<cross_section ID="0" description="Geometrical description of one tank cross section.">
<name description="Name of tank cross section.">
<value>front_end_cap</value>
</name>
<position description="Position of tank cross section with regard to the local reference point.">
<x description="Distance between the tank cross section and the local reference point in x-direction.">
<value>-0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the tank cross section and the local reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</y>
<z description="Distance between the tank cross section and the local reference point in z-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</z>
</position>
<shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
<value>circular</value>
</shape>
<height description="Height of the cross section.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</height>
<width description="Width of the cross section.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</width>
<length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
<value>0.8781485752888233</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</length>
</cross_section>
<cross_section ID="1" description="Geometrical description of one tank cross section.">
<name description="Name of tank cross section.">
<value>front_tank_section</value>
</name>
<position description="Position of tank cross section with regard to the local reference point.">
<x description="Distance between the tank cross section and the local reference point in x-direction.">
<value>-0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the tank cross section and the local reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</y>
<z description="Distance between the tank cross section and the local reference point in z-direction.">
<value>0.878148575</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</z>
</position>
<shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
<value>circular</value>
</shape>
<height description="Height of the cross section.">
<value>3.4359306216476657</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</height>
<width description="Width of the cross section.">
<value>3.4359306216476657</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</width>
<length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</length>
</cross_section>
<cross_section ID="2" description="Geometrical description of one tank cross section.">
<name description="Name of tank cross section.">
<value>rear_tank_section</value>
</name>
<position description="Position of tank cross section with regard to the local reference point.">
<x description="Distance between the tank cross section and the local reference point in x-direction.">
<value>-0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the tank cross section and the local reference point in y-direction.">
<value>0.045861048</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</y>
<z description="Distance between the tank cross section and the local reference point in z-direction.">
<value>2.358148575</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</z>
</position>
<shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
<value>circular</value>
</shape>
<height description="Height of the cross section.">
<value>3.2200412567453918</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</height>
<width description="Width of the cross section.">
<value>3.2200412567453918</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</width>
<length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</length>
</cross_section>
<cross_section ID="3" description="Geometrical description of one tank cross section.">
<name description="Name of tank cross section.">
<value>rear_end_cap</value>
</name>
<position description="Position of tank cross section with regard to the local reference point.">
<x description="Distance between the tank cross section and the local reference point in x-direction.">
<value>-0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the tank cross section and the local reference point in y-direction.">
<value>0.045861048</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</y>
<z description="Distance between the tank cross section and the local reference point in z-direction.">
<value>3.194522558</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</z>
</position>
<shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
<value>circular</value>
</shape>
<height description="Height of the cross section.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</height>
<width description="Width of the cross section.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</width>
<length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
<value>-0.8363739831802333</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</length>
</cross_section>
</geometry>
<mass_breakdown description="Mass breakdown of one tank.">
<tank_insulation description="Mass breakdown of the tank insulation.">
<component_mass ID="0" description="Mass of a single component of the tank insulation.">
<name description="Name of the tank insulation component.">
<value>insulation</value>
</name>
<mass description="Mass of the tank insulation component.">
<value>301.2756208825662</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="1" description="Mass of a single component of the tank insulation.">
<name description="Name of the tank insulation component.">
<value>vapor_barrier</value>
</name>
<mass description="Mass of the tank insulation component.">
<value>24.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
</tank_insulation>
<tank_structure description="Mass breakdown of the tank structure.">
<component_mass ID="0" description="Mass of a single component of the tank structure.">
<name description="Name of the tank structure component.">
<value>wall</value>
</name>
<mass description="Mass of the tank structure component.">
<value>341.55512062185664</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="1" description="Mass of a single component of the tank structure.">
<name description="Name of the tank structure component.">
<value>pumps</value>
</name>
<mass description="Mass of the tank structure component.">
<value>9.26</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="2" description="Mass of a single component of the tank structure.">
<name description="Name of the tank structure component.">
<value>baffle</value>
</name>
<mass description="Mass of the tank structure component.">
<value>45.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
</tank_structure>
</mass_breakdown>
</tank>
<tank ID="1" description="Description of one tank.">
<name description="Name of the tank.">
<value>tank_1</value>
</name>
<designator description="Designator of the tank.">
<value>fuselage_rear</value>
</designator>
<position description="Local reference point, position of one tank wrt. the tank reference point.">
<x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-40</lower_boundary>
<upper_boundary>40</upper_boundary>
</y>
<z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</position>
<direction description="Unit vector according to global coordinate system for direction applied at position.">
<x description="X component of the unit vector.">
<value>1</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</x>
<y description="Y component of the unit vector.">
<value>0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</y>
<z description="Z component of the unit vector.">
<value>0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</z>
</direction>
<mass_properties description="Mass properties of one tank.">
<mass description="Total dry mass of one tank.">
<value>1378.170243280248</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of one tank with regard to its center of gravity.">
<j_xx description="Inertia of the of one tank in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia of the of one tank in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia of the of one tank in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia of one tank in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia of one tank in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia of one tank in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia of one tank in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia of one tank in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia of one tank in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of one tank.">
<x description="Center of gravity in x-direction with regard to the local reference point.">
<value>3.677540451217963</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the local reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-40</lower_boundary>
<upper_boundary>40</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the local reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</center_of_gravity>
<centroid description="Centroid of one tank.">
<x description="Centroid in x-direction with regard to the local reference point.">
<value>3.677540451</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Centroid in y-direction with regard to the local reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-40</lower_boundary>
<upper_boundary>40</upper_boundary>
</y>
<z description="Centroid in z-direction with regard to the local reference point.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-5</lower_boundary>
<upper_boundary>5</upper_boundary>
</z>
</centroid>
</mass_properties>
<maximum_energy_capacity description="Maximum energy capacity of one tank.">
<value>5.160300836e+11</value>
<unit>J</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</maximum_energy_capacity>
<energy_capacity_required_for_mission description="Energy amount required for mission.">
<value>true</value>
</energy_capacity_required_for_mission>
<mass_breakdown description="Mass breakdown of one tank.">
<tank_structure description="Mass breakdown of the tank structure.">
<component_mass ID="0" description="Mass of a single component of the tank structure.">
<name description="Name of the tank structure component.">
<value>wall</value>
</name>
<mass description="Mass of the tank structure component.">
<value>769.6176545771676</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="1" description="Mass of a single component of the tank structure.">
<name description="Name of the tank structure component.">
<value>pumps</value>
</name>
<mass description="Mass of the tank structure component.">
<value>9.26</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="2" description="Mass of a single component of the tank structure.">
<name description="Name of the tank structure component.">
<value>baffle</value>
</name>
<mass description="Mass of the tank structure component.">
<value>45.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
</tank_structure>
<tank_insulation description="Mass breakdown of the tank insulation.">
<component_mass ID="0" description="Mass of a single component of the tank insulation.">
<name description="Name of the tank insulation component.">
<value>insulation</value>
</name>
<mass description="Mass of the tank insulation component.">
<value>530.2925887030806</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
<component_mass ID="1" description="Mass of a single component of the tank insulation.">
<name description="Name of the tank insulation component.">
<value>vapor_barrier</value>
</name>
<mass description="Mass of the tank insulation component.">
<value>24.0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</mass>
</component_mass>
</tank_insulation>
</mass_breakdown>
<geometry description="Geometrical description of one tank.">
<cross_section ID="0" description="Geometrical description of one tank cross section.">
<name description="Name of tank cross section.">
<value>front_end_cap</value>
</name>
<position description="Position of tank cross section with regard to the local reference point.">
<x description="Distance between the tank cross section and the local reference point in x-direction.">
<value>-0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the tank cross section and the local reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</y>
<z description="Distance between the tank cross section and the local reference point in z-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</z>
</position>
<shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
<value>circular</value>
</shape>
<height description="Height of the cross section.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</height>
<width description="Width of the cross section.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</width>
<length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
<value>0.902540451218</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</length>
</cross_section>
<cross_section ID="1" description="Geometrical description of one tank cross section.">
<name description="Name of tank cross section.">
<value>front_tank_section</value>
</name>
<position description="Position of tank cross section with regard to the local reference point.">
<x description="Distance between the tank cross section and the local reference point in x-direction.">
<value>-0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the tank cross section and the local reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</y>
<z description="Distance between the tank cross section and the local reference point in z-direction.">
<value>0.902540451</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</z>
</position>
<shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
<value>circular</value>
</shape>
<height description="Height of the cross section.">
<value>3.5619868279999998</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</height>
<width description="Width of the cross section.">
<value>3.5619868279999998</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</width>
<length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</length>
</cross_section>
<cross_section ID="2" description="Geometrical description of one tank cross section.">
<name description="Name of tank cross section.">
<value>rear_tank_section</value>
</name>
<position description="Position of tank cross section with regard to the local reference point.">
<x description="Distance between the tank cross section and the local reference point in x-direction.">
<value>-0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the tank cross section and the local reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</y>
<z description="Distance between the tank cross section and the local reference point in z-direction.">
<value>6.452540451</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</z>
</position>
<shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
<value>circular</value>
</shape>
<height description="Height of the cross section.">
<value>3.5619868279999998</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</height>
<width description="Width of the cross section.">
<value>3.5619868279999998</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</width>
<length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</length>
</cross_section>
<cross_section ID="3" description="Geometrical description of one tank cross section.">
<name description="Name of tank cross section.">
<value>rear_end_cap</value>
</name>
<position description="Position of tank cross section with regard to the local reference point.">
<x description="Distance between the tank cross section and the local reference point in x-direction.">
<value>-0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</x>
<y description="Distance between the tank cross section and the local reference point in y-direction.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</y>
<z description="Distance between the tank cross section and the local reference point in z-direction.">
<value>7.355080902</value>
<unit>m</unit>
<lower_boundary>-80</lower_boundary>
<upper_boundary>80</upper_boundary>
</z>
</position>
<shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
<value>circular</value>
</shape>
<height description="Height of the cross section.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</height>
<width description="Width of the cross section.">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</width>
<length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
<value>-0.902540451218</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</length>
</cross_section>
</geometry>
</tank>
</specific>
</tank>
<landing_gear description="Geometric description of the aircraft undercarriage." tool_level="3">
<position description="Position of the total undercarriage arrangement with regard to the global reference point.">
<x description="Distance in x direction with regard to the global reference point. (total undercarriage arrangement)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Distance in y direction with regard to the global reference point. (total undercarriage arrangement)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-25</lower_boundary>
<upper_boundary>25</upper_boundary>
</y>
<z description="Distance in z direction with regard to the global reference point. (total undercarriage arrangement)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of the total undercarriage arrangement.">
<mass description="Mass of the total undercarriage arrangement.">
<value>2933.4069</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</mass>
<inertia description="Inertia of the total undercarriage arrangement with regard to the total center of gravity.">
<j_xx description="Inertia of the total undercarriage arrangement in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia of the total undercarriage arrangement in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia of the total undercarriage arrangement in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia of the total undercarriage arrangement in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia of the total undercarriage arrangement in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia of the total undercarriage arrangement in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia of the total undercarriage arrangement in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia of the total undercarriage arrangement in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia of the total undercarriage arrangement in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of the total undercarriage arrangement.">
<x description="Center of gravity in x-direction with regard to the global reference point. (total undercarriage arrangement)">
<value>20.1679</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in y-direction with regard to the global reference point. (total undercarriage arrangement)">
<value>0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in z-direction with regard to the global reference point. (total undercarriage arrangement)">
<value>-1.6454</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<aircraft_classification_number description="Aircraft classification number for the total undercarriage arrangement. (CBR = [3, 6, 10, 15])">
<value>[53.5, 47.6, 43.5, 41.6]</value>
</aircraft_classification_number>
<specific description="Landing gear specific output parameter.">
<geometry description="Geometry description of the entire landing gear.">
<landing_gear_assembly ID="0" description="Geometrical description of one entire landing gear leg.">
<name description="Name of the landing gear leg.">
<value>nose_gear_assembly</value>
</name>
<position description="Position of one entire landing gear leg with regard to the landing gear global position.">
<x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
<value>5.2</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
<value>-1.6572</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of one entire landing gear leg.">
<mass description="Mass of one entire landing gear leg.">
<value>441.3324</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10000</upper_boundary>
</mass>
<inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
<j_xx description="Inertia of one entire landing gear leg in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia of one entire landing gear leg in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia of one entire landing gear leg in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia of one entire landing gear leg in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia of one entire landing gear leg in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia of one entire landing gear leg in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia of one entire landing gear leg in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia of one entire landing gear leg in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia of one entire landing gear leg in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of one entire landing gear leg.">
<x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
<value>-16.0097</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
<value>0.0118</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
<strut_diameter description="Diameter of the landing gear strut">
<value>0.2248</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.0</upper_boundary>
</strut_diameter>
<strut_length description="Length of the landing gear strut">
<value>2.0835</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</strut_length>
<tire_description ID="0" description="Description of one tire of the wheel group.">
<name description="Name of the tire type.">
<value>APS01203</value>
</name>
<position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
<x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</x>
<y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
<value>-0.3372</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</y>
<z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>-2.0835</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<tire_diameter description="Diameter of one tire of the wheel group.">
<value>0.7699</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>2</upper_boundary>
</tire_diameter>
<tire_section_width description="Width at the shoulder of a tire of the wheel group.">
<value>0.2248</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</tire_section_width>
</tire_description>
<tire_description ID="1" description="Description of one tire of the wheel group.">
<name description="Name of the tire type.">
<value>APS01203</value>
</name>
<position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
<x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</x>
<y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
<value>0.3372</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</y>
<z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>-2.0835</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<tire_diameter description="Diameter of one tire of the wheel group.">
<value>0.7699</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>2</upper_boundary>
</tire_diameter>
<tire_section_width description="Width at the shoulder of a tire of the wheel group.">
<value>0.2248</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</tire_section_width>
</tire_description>
</assembly_components>
</landing_gear_assembly>
<landing_gear_assembly ID="1" description="Geometrical description of one entire landing gear leg.">
<name description="Name of the landing gear leg.">
<value>right_main_gear_outer_strut</value>
</name>
<position description="Position of one entire landing gear leg with regard to the landing gear global position.">
<x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
<value>23.0031</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
<value>4.4813</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
<value>-0.8565</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of one entire landing gear leg.">
<mass description="Mass of one entire landing gear leg.">
<value>1246.0373</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10000</upper_boundary>
</mass>
<inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
<j_xx description="Inertia of one entire landing gear leg in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia of one entire landing gear leg in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia of one entire landing gear leg in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia of one entire landing gear leg in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia of one entire landing gear leg in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia of one entire landing gear leg in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia of one entire landing gear leg in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia of one entire landing gear leg in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia of one entire landing gear leg in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of one entire landing gear leg.">
<x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
<value>1.3931</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
<value>4.4813</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
<value>0.2162</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
<strut_diameter description="Diameter of the landing gear strut">
<value>0.2322</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.0</upper_boundary>
</strut_diameter>
<strut_length description="Length of the landing gear strut">
<value>2.8842</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</strut_length>
<tire_description ID="0" description="Description of one tire of the wheel group.">
<name description="Name of the tire type.">
<value>APS00524-E</value>
</name>
<position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
<x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</x>
<y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
<value>-0.4635</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</y>
<z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>-2.8842</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<tire_diameter description="Diameter of one tire of the wheel group.">
<value>1.1493</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>2</upper_boundary>
</tire_diameter>
<tire_section_width description="Width at the shoulder of a tire of the wheel group.">
<value>0.4064</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</tire_section_width>
</tire_description>
<tire_description ID="1" description="Description of one tire of the wheel group.">
<name description="Name of the tire type.">
<value>APS00524-E</value>
</name>
<position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
<x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</x>
<y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
<value>0.4635</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</y>
<z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>-2.8842</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<tire_diameter description="Diameter of one tire of the wheel group.">
<value>1.1493</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>2</upper_boundary>
</tire_diameter>
<tire_section_width description="Width at the shoulder of a tire of the wheel group.">
<value>0.4064</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</tire_section_width>
</tire_description>
</assembly_components>
</landing_gear_assembly>
<landing_gear_assembly ID="2" description="Geometrical description of one entire landing gear leg.">
<name description="Name of the landing gear leg.">
<value>left_main_gear_outer_strut</value>
</name>
<position description="Position of one entire landing gear leg with regard to the landing gear global position.">
<x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
<value>23.0031</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
<value>-4.4813</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
<value>-0.8565</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<mass_properties description="Mass properties of one entire landing gear leg.">
<mass description="Mass of one entire landing gear leg.">
<value>1246.0373</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10000</upper_boundary>
</mass>
<inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
<j_xx description="Inertia of one entire landing gear leg in x.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xx>
<j_yy description="Inertia of one entire landing gear leg in y.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yy>
<j_zz description="Inertia of one entire landing gear leg in z.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zz>
<j_xy description="Inertia of one entire landing gear leg in xy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xy>
<j_xz description="Inertia of one entire landing gear leg in xz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_xz>
<j_yx description="Inertia of one entire landing gear leg in yx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yx>
<j_yz description="Inertia of one entire landing gear leg in yz.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_yz>
<j_zx description="Inertia of one entire landing gear leg in zx.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zx>
<j_zy description="Inertia of one entire landing gear leg in zy.">
<value>0.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</j_zy>
</inertia>
<center_of_gravity description="Center of gravity of one entire landing gear leg.">
<x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
<value>1.3931</value>
<unit>m</unit>
<lower_boundary>-100</lower_boundary>
<upper_boundary>100</upper_boundary>
</x>
<y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
<value>4.4813</value>
<unit>m</unit>
<lower_boundary>-50</lower_boundary>
<upper_boundary>50</upper_boundary>
</y>
<z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
<value>0.2162</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</center_of_gravity>
</mass_properties>
<assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
<strut_diameter description="Diameter of the landing gear strut">
<value>0.2322</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1.0</upper_boundary>
</strut_diameter>
<strut_length description="Length of the landing gear strut">
<value>2.8842</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10</upper_boundary>
</strut_length>
<tire_description ID="0" description="Description of one tire of the wheel group.">
<name description="Name of the tire type.">
<value>APS00524-E</value>
</name>
<position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
<x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</x>
<y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
<value>-0.4635</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</y>
<z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>-2.8842</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<tire_diameter description="Diameter of one tire of the wheel group.">
<value>1.1493</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>2</upper_boundary>
</tire_diameter>
<tire_section_width description="Width at the shoulder of a tire of the wheel group.">
<value>0.4064</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</tire_section_width>
</tire_description>
<tire_description ID="1" description="Description of one tire of the wheel group.">
<name description="Name of the tire type.">
<value>APS00524-E</value>
</name>
<position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
<x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>0.0</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</x>
<y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
<value>0.4635</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</y>
<z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
<value>-2.8842</value>
<unit>m</unit>
<lower_boundary>-10</lower_boundary>
<upper_boundary>10</upper_boundary>
</z>
</position>
<tire_diameter description="Diameter of one tire of the wheel group.">
<value>1.1493</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>2</upper_boundary>
</tire_diameter>
<tire_section_width description="Width at the shoulder of a tire of the wheel group.">
<value>0.4064</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</tire_section_width>
</tire_description>
</assembly_components>
</landing_gear_assembly>
</geometry>
</specific>
</landing_gear>
</component_design>
<sizing_point>
<thrust_to_weight description="Total thrust (kN) divided by maximum aircraft weight (kN)">
<value>0.3364390052</value>
<unit>1</unit>
<lower_boundary>-1.797693135e+308</lower_boundary>
<upper_boundary>1.797693135e+308</upper_boundary>
</thrust_to_weight>
<wing_loading description="Maximum takeoff mass (MTOM) divided by wing area (Sref)">
<value>560</value>
<unit>kg/m^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
</wing_loading>
</sizing_point>
<assessment description="Assessment data">
<performance description="Assessment of performance values">
<takeoff description="Takeoff assessment">
<takeoff_distance_normal_safety description="Takeoff distance at Sea Level for MTOM and (ISA + deltaISA)-Conditions(calculated by mission_analysis using missionDesign.xml settings) with all engines operating (AEO)">
<value>907.8759565</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>5000</upper_boundary>
</takeoff_distance_normal_safety>
<lift_off_speed_velocity description="Lift off velocity">
<value>65.20930452</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>400</upper_boundary>
</lift_off_speed_velocity>
<takeoff_safety_speed description="Take off safety speed (V2)">
<value>65.20930452</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>200</upper_boundary>
</takeoff_safety_speed>
<final_takeoff_speed description="Final take off speed">
<value>95.38595077</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>200</upper_boundary>
</final_takeoff_speed>
<time_to_screen_height description="Time to screen height">
<value>28.52834443</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>3600</upper_boundary>
</time_to_screen_height>
<climb_or_descend_segment_climb_gradient description="Climb or descend in second segment">
<value>3.93217426</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100</upper_boundary>
</climb_or_descend_segment_climb_gradient>
<final_segment_climb_gradient description="Climb gradient in final segment">
<value>3.93217426</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100</upper_boundary>
</final_segment_climb_gradient>
</takeoff>
<altitude description="Assessment of altitude related values">
<maximum_operating_altitude description="Maximum operating altitude (100 ft/min rate of climb)">
<value>12545.57013</value>
<unit>m</unit>
<lower_boundary>4500</lower_boundary>
<upper_boundary>20000</upper_boundary>
</maximum_operating_altitude>
<maximum_ceiling_altitude description="Maximum operating altitude (50 ft/min rate of climb)">
<value>12660.55488</value>
<unit>m</unit>
<lower_boundary>4500</lower_boundary>
<upper_boundary>20000</upper_boundary>
</maximum_ceiling_altitude>
<maximum_altitude_one_engine_inoperative description="Maximum operating altitude with one engine inoperative (100 ft/min rate of climb)">
<value>6415.414758</value>
<unit>m</unit>
<lower_boundary>1500</lower_boundary>
<upper_boundary>12000</upper_boundary>
</maximum_altitude_one_engine_inoperative>
</altitude>
<climb description="Assessment of the climb segment">
<design_time_to_climb description="Time needed to climb from 1500ft to ICA (ISA + deltaISA)">
<value>1050.354193</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>7200</upper_boundary>
</design_time_to_climb>
<time_to_1500ft_ISA description="Time needed to climb from break release to 1500ft (ISA + deltaISA)">
<value>69.18025702</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>7200</upper_boundary>
</time_to_1500ft_ISA>
<time_to_ICA_ISA description="Time needed to climb from break release to ICA (ISA + deltaISA)">
<value>1119.53445</value>
<unit>s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>7200</upper_boundary>
</time_to_ICA_ISA>
<range_to_ICA_ISA description="Range needed to climb from break release to ICA (ISA + deltaISA)">
<value>208170.2184</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>500000</upper_boundary>
</range_to_ICA_ISA>
<fuel_to_ICA_ISA description="Fuel mass needed to climb from break release to ICA (ISA + deltaISA)">
<value>502.5839811</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>10000</upper_boundary>
</fuel_to_ICA_ISA>
</climb>
<speed>
<maximum_operating_mach_number description="Maximum operating mach number">
<value>0.82</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</maximum_operating_mach_number>
<maximum_operating_velocity description="Maximum operating velocity">
<value>180</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>400</upper_boundary>
</maximum_operating_velocity>
<dive_mach_number description="Maximum dive mach number">
<value>0.902</value>
<unit>1</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1</upper_boundary>
</dive_mach_number>
<dive_velocity description="Dive velocity">
<value>198</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>400</upper_boundary>
</dive_velocity>
<one_g_stall_speed_velocity description="One g stall speed">
<value>74.39186581</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>400</upper_boundary>
</one_g_stall_speed_velocity>
</speed>
<landing>
<needed_runway_length description="Needed runway length">
<value>1495.151103</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>100000</upper_boundary>
</needed_runway_length>
<approach_speed description="Approach speed">
<value>60.48885847</value>
<unit>m/s</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>1000</upper_boundary>
</approach_speed>
</landing>
<range>
<range_max_payload_at_maximum_takeoff_mass description="Range at max payload at maximum take off mass">
<value>0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</range_max_payload_at_maximum_takeoff_mass>
<range_max_fuel_at_maximum_takeoff_mass description="Range at max fuel at maximum take off mass">
<value>0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</range_max_fuel_at_maximum_takeoff_mass>
<payload_maximum_fuel_at_maximum_takeoff_mass description="Payload at maximum fuel at maximum takeoff mass">
<value>0</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</payload_maximum_fuel_at_maximum_takeoff_mass>
<range_maximum_fuel_empty description="Range at maximum fuel empty">
<value>0</value>
<unit>m</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</range_maximum_fuel_empty>
</range>
</performance>
<ecological_assessment description="Ecological assessment data" />
<operating_cost_estimation_tu_berlin description="Operating costs (sum of direct and indirect operating costs)" tool_level="2">
<direct_operating_costs description="Direct operating costs (sum of route independent and route dependent costs)">
<direct_operating_costs_annual description="Direct operating costs (DOC) per year">
<value>30</value>
<unit>EUR/y</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</direct_operating_costs_annual>
</direct_operating_costs>
<indirect_operating_costs description="Indirect operating costs (IOC)">
<indirect_operating_costs_annual description="Indirect operating costs (IOC) per year">
<value>40</value>
<unit>EUR/y</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
</indirect_operating_costs_annual>
</indirect_operating_costs>
</operating_cost_estimation_tu_berlin>
</assessment>
<requirement_compliance description="Compliance of given requirements">
<top_level_aircraft_requirements description="Compliance of top level aircraft requirements">
<initial_cruise_altitude description="Compliance check of the initial cruise altitude.">
<maintainable description="Value shows if the requirement can be achieved by the aircraft.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</initial_cruise_altitude>
<initial_cruise_mach_number description="Compliance check of the initial cruise mach number.">
<maintainable description="Value shows if the requirement can be achieved by the aircraft.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</initial_cruise_mach_number>
<maximum_operating_altitude description="Compliance check of the maximum operating altitude.">
<maintainable description="Value shows if the requirement can be achieved by the aircraft.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</maximum_operating_altitude>
<maximum_altitude_one_engine_inoperative description="Compliance check of the maximum altitude one engine inoperative.">
<maintainable description="Value shows if the requirement can be achieved by the aircraft.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</maximum_altitude_one_engine_inoperative>
<design_time_to_climb description="Compliance check of the design time to climb.">
<maintainable description="Value shows if the requirement can be achieved by the aircraft.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</design_time_to_climb>
<design_takeoff_distance description="Compliance check of the design takeoff distance.">
<maintainable description="Switch indicating if design takeoff distance can be maintained.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</design_takeoff_distance>
<design_landing_field_length description="Compliance check of the design landing field length.">
<maintainable description="Switch indicating if landing field length can be maintained.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</design_landing_field_length>
<design_approach_speed description="Compliance check of the design approach speed.">
<maintainable description="Switch indicating if approach speed can be maintained.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</design_approach_speed>
<span_limit>
<maintainable description="Switch indicating if the span limit according to ICAO aerodrome ref code is maintained.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</span_limit>
</top_level_aircraft_requirements>
<certification>
<climb_gradient_of_second_takeoff_segment>
<maintainable description="Switch indicating if climb gradient of second takeoff segment can be maintained.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</climb_gradient_of_second_takeoff_segment>
<climb_gradient_of_final_takeoff_segment>
<maintainable description="Switch indicating if climb gradient of final takeoff segment can be maintained.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</climb_gradient_of_final_takeoff_segment>
<climb_gradient_approach_one_engine_inoperative>
<maintainable description="Switch indicating if climb gradient approach one engine inoperative can be maintained.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</climb_gradient_approach_one_engine_inoperative>
<climb_gradient_all_engines_operative>
<maintainable description="Switch indicating if climb gradient with all engines operative can be maintained.">
<value>true</value>
</maintainable>
<checked description="Indicates if the value has been checked against the requirement.">
<value>true</value>
</checked>
</climb_gradient_all_engines_operative>
</certification>
</requirement_compliance>
</aircraft_exchange_file>