diff --git a/.gitignore b/.gitignore index 89988e792434ebd924eb04146d7dc526fca8a333..adc07191da96ad6c2171452348da6ada8beebf46 100644 --- a/.gitignore +++ b/.gitignore @@ -3,7 +3,6 @@ *.o obj/ *.res -projects/ # IDE Files .vscode diff --git a/projects/newFormat-CSMR-2020.xml b/projects/newFormat-CSMR-2020.xml new file mode 100644 index 0000000000000000000000000000000000000000..925455677c2ec5c63db49b40a49280c4566277ae --- /dev/null +++ b/projects/newFormat-CSMR-2020.xml @@ -0,0 +1,10198 @@ +<aircraft_exchange_file> + <requirements_and_specifications description="Requirements and specifications"> + <general description="General aircraft information"> + <type description="Aircraft type"> + <value>CeRAS</value> + </type> + <model description="Model - Version"> + <value>SMR-2020</value> + </model> + </general> + <mission_files description="Name of xml files which are located in the missionData directory and contain the flight phase data" tool_level="0"> + <design_mission_file description="Name of the design mission xml"> + <value>design_mission.xml</value> + </design_mission_file> + <study_mission_file description="Name of the study mission xml"> + <value>study_mission.xml</value> + </study_mission_file> + <requirements_mission_file description="Name of the requirements mission xml"> + <value>requirements_mission.xml</value> + </requirements_mission_file> + </mission_files> + <design_specification description="Design specification"> + <configuration description="Configuration information"> + <aerodynamic_technologies description="Integration of aerodynamic technologies on the aircraft: true / false"> + <value>false</value> + </aerodynamic_technologies> + <configuration_type description="aircraft configuration: tube_and_wing / blended_wing_body"> + <value>tube_and_wing</value> + </configuration_type> + <fuselage_definition description="Design description of the fuselage."> + <fuselage_type description="Fuselage type: single_aisle / wide_body"> + <value>single_aisle</value> + </fuselage_type> + <fuselage_pressurization description="Switch to select a pressurized fuselage. (true: pressurized fuselage, false: non pressurized fuselage)"> + <value>true</value> + </fuselage_pressurization> + <blended_wing_body_configuration description="Additional design description for blended wing body configurations."> + <number_of_payload_tubes description="Number of fuselage tubes for blendend wing body configurations. For tube and wing configuration is set to 1."> + <value>1</value> + <unit>1</unit> + <default>1</default> + <lower_boundary>1</lower_boundary> + <upper_boundary>5</upper_boundary> + </number_of_payload_tubes> + <center_body_wing_sweep description="Sweep of the leading edge of the center body."> + <value>60</value> + <unit>degree</unit> + <default>60</default> + <lower_boundary>0</lower_boundary> + <upper_boundary>75</upper_boundary> + <center_body_wing_sweep_tolerance Desc="Permissible deviation of the actual from the desired leading edge sweep of the center body."> + <value>5</value> + <unit>degree</unit> + <default>5</default> + <lower_boundary>0</lower_boundary> + <upper_boundary>15</upper_boundary> + </center_body_wing_sweep_tolerance> + </center_body_wing_sweep> + </blended_wing_body_configuration> + </fuselage_definition> + <wing_definition description="Definitions for wing design"> + <mounting description="wing mounting for tube_and_wing configuration (ignored at blended_wing_body) - low / mid / high"> + <value>low</value> + </mounting> + </wing_definition> + <empennage_definition description="Definitions for empennage design"> + <empennage_type description="tube_and_wing configuration: conventional - blended_wing_body: vertical_tails"> + <value>conventional</value> + </empennage_type> + </empennage_definition> + <undercarriage_definition description="Design description of the undercarriage."> + <main_gear_mounting description="Mounting position of the main landing gear: wing_mounted / fuselage_mounted."> + <value>wing_mounted</value> + </main_gear_mounting> + <undercarriage_retractability description="Switch to set retractability of landing gear: retractable / non_retractable."> + <value>retractable</value> + </undercarriage_retractability> + </undercarriage_definition> + <tank_definition description="Energy tanks information"> + <tank ID="0" description="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: fuselage, wing, horizontal_stabilizer"> + <value>wing</value> + </location> + <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total"> + <value>inner_left</value> + </position> + <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks."> + <value>0.0</value> + <unit>1</unit> + <lower_boundary>0.0</lower_boundary> + <upper_boundary>1.0</upper_boundary> + </energy_share> + </tank> + <tank ID="1" description="Outer left tank"> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer"> + <value>wing</value> + </location> + <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total"> + <value>outer_left</value> + </position> + <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks."> + <value>0.0</value> + <unit>1</unit> + <lower_boundary>0.0</lower_boundary> + <upper_boundary>1.0</upper_boundary> + </energy_share> + </tank> + <tank ID="2" description="Inner right tank"> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer"> + <value>wing</value> + </location> + <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total"> + <value>inner_right</value> + </position> + <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks."> + <value>0.0</value> + <unit>1</unit> + <lower_boundary>0.0</lower_boundary> + <upper_boundary>1.0</upper_boundary> + </energy_share> + </tank> + <tank ID="3" description="Outer right tank"> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer"> + <value>wing</value> + </location> + <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total"> + <value>outer_right</value> + </position> + <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks."> + <value>0.0</value> + <unit>1</unit> + <lower_boundary>0.0</lower_boundary> + <upper_boundary>1.0</upper_boundary> + </energy_share> + </tank> + <tank ID="4" description="Center wing tank"> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer"> + <value>wing</value> + </location> + <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total"> + <value>center</value> + </position> + <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks."> + <value>0.0</value> + <unit>1</unit> + <lower_boundary>0.0</lower_boundary> + <upper_boundary>1.0</upper_boundary> + </energy_share> + </tank> + <tank ID="5" description="Additional center 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: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total"> + <value>center</value> + </position> + <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks."> + <value>0.0</value> + <unit>1</unit> + <lower_boundary>0.0</lower_boundary> + <upper_boundary>1.0</upper_boundary> + </energy_share> + </tank> + <tank ID="6" description="Trim 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>horizontal_stabilizer</value> + </location> + <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total"> + <value>total</value> + </position> + <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks."> + <value>0.0</value> + <unit>1</unit> + <lower_boundary>0.0</lower_boundary> + <upper_boundary>1.0</upper_boundary> + </energy_share> + </tank> + </tank_definition> + <loads description="Loads information"> + <design_load_factor description="design load factor n"> + <maximum description="maximum design load factor n"> + <value>2.5</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>4</upper_boundary> + </maximum> + <minimum description="maximum design load factor n"> + <value>-1.0</value> + <unit>1</unit> + <lower_boundary>-2.0</lower_boundary> + <upper_boundary>0.0</upper_boundary> + </minimum> + <maneuver description="standard maneuver load factor for e.g. flare"> + <value>1.1</value> + <unit>1</unit> + <lower_boundary>0.0</lower_boundary> + <upper_boundary>2.0</upper_boundary> + </maneuver> + </design_load_factor> + </loads> + </configuration> + <transport_task 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 a 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. (true: multi passenger deck allowed, false: multi passenger deck denied)"> + <value>false</value> + <default>false</default> + <specific_number_of_passenger_decks> + <value>2</value> + <unit>-</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>3</upper_boundary> + <default>2</default> + </specific_number_of_passenger_decks> + </multi_passenger_deck_layout> + <passenger_class_definition> + <class_distribution description="Relative passenger distribution for the classes: President Class/First Class/Business Class/Premium Economy/Economy. Sum must be equal to 1!"> + <value>0/0/0/0/1</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 / liquid_hydrogen / battery / saf"> + <value>kerosene</value> + </type> + <density description="Energy carrier density."> + <value>785</value> + <unit>kg/m^3</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10000</upper_boundary> + </density> + <volumetric_density description="Volumetric energy density of energy carrier."> + <value>33.833</value> + <unit>J/m^3</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1e+12</upper_boundary> + </volumetric_density> + <gravimetric_density description="Gravimetric energy density of energy carrier."> + <value>43100000</value> + <unit>J/kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1e+12</upper_boundary> + </gravimetric_density> + </energy_carrier> + </energy_carriers> + <propulsion description="Propulsion information"> + <propulsor ID="123" description="Information for specific propulsor"> + <powertrain description="Way the power is generated from the source. Selector: turbo / electric / fuel_cell"> + <value>turbo</value> + </powertrain> + <type description="Type of main thrust generator. Selector: fan / prop"> + <value>fan</value> + </type> + <position description="propulsor position (arrangement order acc to ID order)"> + <parent_component description="position on component. Selector: wing / fuselage / empennage"> + <value>wing</value> + </parent_component> + <x description="x-position (aircraft coordinate system). Selector: front / back"> + <value>front</value> + </x> + <y description="y position (aircraft coordinate system). Selector: left / right"> + <value>left</value> + </y> + <z description="z position (aircraft coordinate system). Selector: over / mid / under / in"> + <value>under</value> + </z> + </position> + <energy_carrier_ID description="see energy carrier specification node"> + <value>999</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + <thrust_share description="Share of this thrust in relation to required aircraft thrust"> + <value>0.5</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </thrust_share> + </propulsor> + <propulsor ID="1" description="Information for specific propulsor"> + <powertrain description="Way the power is generated from the source. Selector: turbo / electric / fuel_cell"> + <value>turbo</value> + </powertrain> + <type description="Type of main thrust generator. Selector: fan / prop"> + <value>fan</value> + </type> + <position description="propulsor position (arrangement order acc to ID order)"> + <parent_component description="position on component. Selector: wing / fuselage / empennage"> + <value>wing</value> + </parent_component> + <x description="x-position (aircraft coordinate system). Selector: front / back"> + <value>front</value> + </x> + <y description="y position (aircraft coordinate system). Selector: left / right"> + <value>right</value> + </y> + <z description="z position (aircraft coordinate system). Selector: over / mid / under / in"> + <value>under</value> + </z> + </position> + <energy_carrier_ID description="see energy carrier specification node"> + <value>888</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="10" description="Information for specific propulsor"> + <powertrain description="Way the power is generated from the source. Selector: turbo / electric / fuel_cell"> + <value>turbo</value> + </powertrain> + <type description="Type of main thrust generator. Selector: fan / prop"> + <value>fan</value> + </type> + <position description="propulsor position (arrangement order acc to ID order)"> + <parent_component description="position on component. Selector: wing / fuselage / empennage"> + <value>wing</value> + </parent_component> + <x description="x-position (aircraft coordinate system). Selector: front / back"> + <value>front</value> + </x> + <y description="y position (aircraft coordinate system). Selector: left / right"> + <value>right</value> + </y> + <z description="z position (aircraft coordinate system). Selector: over / mid / under / in"> + <value>under</value> + </z> + </position> + <energy_carrier_ID description="see energy carrier specification node"> + <value>777</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + <thrust_share description="Share of this thrust in relation to required aircraft thrust"> + <value>0.5</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </thrust_share> + </propulsor> + <energy_provider description="source where energy is coming from per segment"> + <ground description="source where energy is coming from in the ground mission segment"> + <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell"> + <value>turbo</value> + </powertrain> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </ground> + <taxi description="source where energy is coming from in the taxi mission segment"> + <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell"> + <value>turbo</value> + </powertrain> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </taxi> + <takeoff description="source where energy is coming from in the takeoff mission segment"> + <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell"> + <value>turbo</value> + </powertrain> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </takeoff> + <climb description="source where energy is coming from in the climb mission segment"> + <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell"> + <value>turbo</value> + </powertrain> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </climb> + <cruise description="source where energy is coming from in the cruise mission segment"> + <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell"> + <value>turbo</value> + </powertrain> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </cruise> + <descent description="source where energy is coming from in the descent mission segment"> + <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell"> + <value>turbo</value> + </powertrain> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </descent> + <landing description="source where energy is coming from in the landing mission segment"> + <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell"> + <value>turbo</value> + </powertrain> + <energy_carrier_ID description="see energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </landing> + </energy_provider> + </propulsion> + <skinning description="Skinning Information"> + <material description="Material of skinning"> + <value>aluminium2024</value> + </material> + <thickness description="Thickness of skinning"> + <value>0.003</value> + <unit>m</unit> + <lower_boundary>0.0001</lower_boundary> + <upper_boundary>0.1</upper_boundary> + </thickness> + </skinning> + <technology> + <variable_camber description="Switch if variable camber is used"> + <value>false</value> + </variable_camber> + </technology> + </design_specification> + <requirements description="Aircraft design requirements"> + <top_level_aircraft_requirements description="Top level aircraft requirements (TLAR)"> + <maximum_structrual_payload_mass description="Maximum structual payload mass which can be carried by the aircraft (e.g. for short trips)"> + <value>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 landiung 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>3CIIIB</value> + </icao_aerodrome_reference_code> + <flight_envelope description="Maxima of design flight envelope"> + <maximum_operating_mach_number description="Maximum operating mach number"> + <value>0.82</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </maximum_operating_mach_number> + <maximum_operating_velocity description="Maximum operating speed (maximum dynamic pressure)"> + <value>180</value> + <unit>m/s</unit> + <lower_boundary>50</lower_boundary> + <upper_boundary>250</upper_boundary> + </maximum_operating_velocity> + <maximum_approach_speed description="Maximum allowed approach speed."> + <value>67.65</value> + <unit>m/s</unit> + <lower_boundary>50</lower_boundary> + <upper_boundary>90</upper_boundary> + </maximum_approach_speed> + <maximum_operating_altitude description="Maximum operating altitude"> + <value>12192</value> + <unit>m</unit> + <lower_boundary>4500</lower_boundary> + <upper_boundary>20000</upper_boundary> + </maximum_operating_altitude> + <maximum_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_descend_segment_gradient description="climb / descend segment gradient"> + <value>0.024</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </climb_or_descend_segment_gradient> + </flight_envelope> + <pavement_classification_number description="Runway pavment classification number (PCN) - limits the maximum allowed aircraft classification number of undercarriage."> + <value>55</value> + <unit>1</unit> + <lower_boundary>5</lower_boundary> + <upper_boundary>120</upper_boundary> + </pavement_classification_number> + <design_mission description="Requirements regarding the design mission"> + <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)"> + <value>0</value> + <unit>K</unit> + <lower_boundary>-100</lower_boundary> + <upper_boundary>100</upper_boundary> + </delta_ISA> + <range description="Target range for the specified mission"> + <value>4537400</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>20000000</upper_boundary> + </range> + <contingency description="Reserved Fuel Percentage"> + <value>0.06</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>0.08</upper_boundary> + </contingency> + <alt_dist description="Reserved fuel - alternate distance"> + <value>370400</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>926000</upper_boundary> + </alt_dist> + <loiter_time description="Reserved fuel - loiter time in seconds"> + <value>1800</value> + <unit>s</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>3600</upper_boundary> + </loiter_time> + <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise."> + <value>0.78</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </initial_cruise_mach_number> + <initial_cruise_altitude description="Initial cruise altitude (ICA) at top of descent. May be altered during cruise."> + <value>10058.4</value> + <unit>m</unit> + <lower_boundary>1000</lower_boundary> + <upper_boundary>20000</upper_boundary> + </initial_cruise_altitude> + <climb_speed_schedule description="Climb speed for different altitudes"> + <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)"> + <value>128.6112</value> + <unit>m/s</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>250</upper_boundary> + </climb_speed_below_FL100> + <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)"> + <value>154.3334</value> + <unit>m/s</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>250</upper_boundary> + </climb_speed_above_FL100> + <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number"> + <value>-0.02</value> + <unit>1</unit> + <lower_boundary>-0.3</lower_boundary> + <upper_boundary>0.01</upper_boundary> + </delta_mach_climb_cruise> + </climb_speed_schedule> + <descent_speed_schedule description="Descent speed for different altitudes"> + <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)"> + <value>128.6112</value> + <unit>m/s</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>250</upper_boundary> + </descent_speed_below_FL100> + <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)"> + <value>154.3334</value> + <unit>m/s</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>250</upper_boundary> + </descent_speed_above_FL100> + </descent_speed_schedule> + <time_to_climb description="Time the aircraft takes to climb to cruise altitude"> + <value>2100</value> + <unit>s</unit> + <lower_boundary>600</lower_boundary> + <upper_boundary>3600</upper_boundary> + </time_to_climb> + <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)"> + <fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)"> + <value>mode_0</value> + </fuel_estimation_selector> + </fuel_planning> + </design_mission> + <study_mission description="Requirements regarding the study mission"> + <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)"> + <value>0</value> + <unit>K</unit> + <lower_boundary>-100</lower_boundary> + <upper_boundary>100</upper_boundary> + </delta_ISA> + <range description="Target range for the specified mission"> + <value>1481600</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>20000000</upper_boundary> + </range> + <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise."> + <value>0.78</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </initial_cruise_mach_number> + <initial_cruise_altitude description="Initial cruise altitude at top of descent. May be altered during cruise."> + <value>10668</value> + <unit>m</unit> + <lower_boundary>1000</lower_boundary> + <upper_boundary>20000</upper_boundary> + </initial_cruise_altitude> + <climb_speed_schedule description="Climb speed for different altitudes"> + <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)"> + <value>128.6112</value> + <unit>m/s</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>250</upper_boundary> + </climb_speed_below_FL100> + <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)"> + <value>154.3334</value> + <unit>m/s</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>250</upper_boundary> + </climb_speed_above_FL100> + <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number"> + <value>-0.02</value> + <unit>1</unit> + <lower_boundary>-0.3</lower_boundary> + <upper_boundary>0.01</upper_boundary> + </delta_mach_climb_cruise> + </climb_speed_schedule> + <descent_speed_schedule description="Descent speed for different altitudes"> + <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)"> + <value>128.6112</value> + <unit>m/s</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>250</upper_boundary> + </descent_speed_below_FL100> + <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)"> + <value>154.3334</value> + <unit>m/s</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>250</upper_boundary> + </descent_speed_above_FL100> + </descent_speed_schedule> + <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)"> + <fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)"> + <value>mode_0</value> + </fuel_estimation_selector> + </fuel_planning> + <payload_fractions description="Set the fraction of different design payload values for the study mission"> + <cargo_fraction description="Fraction of the design cargo mass which is used for the study mission"> + <value>0.75</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </cargo_fraction> + <passenger_mass_fraction description="Fraction of the design passenger mass which is used for the study mission"> + <value>0.75</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </passenger_mass_fraction> + </payload_fractions> + </study_mission> + </top_level_aircraft_requirements> + <additional_requirements description="Additional requirements"> + <landing_gear description="Landing gear requirements and operational conditions"> + <friction_coefficient description="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05"> + <value>0.03</value> + <default>0.03</default> + <unit>1</unit> + <lower_boundary>0.02</lower_boundary> + <upper_boundary>0.08</upper_boundary> + </friction_coefficient> + <breaking_coefficient description="Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189"> + <value>0.34189</value> + <default>0.34189</default> + <unit>1</unit> + <lower_boundary>0.06</lower_boundary> + <upper_boundary>0.5</upper_boundary> + </breaking_coefficient> + </landing_gear> + </additional_requirements> + </requirements> + <assessment_scenario description="Scenario for ecological and economical assessment"> + <flights_per_year description="Number of flights per year"> + <value>2227</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>4000</upper_boundary> + </flights_per_year> + <duration_operation description="Operating years of aircraft"> + <value>25</value> + <unit>a</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>50</upper_boundary> + </duration_operation> + </assessment_scenario> + </requirements_and_specifications> + <analysis> + <masses_cg_inertia description="Masses, Center of Gravity, Inertias." tool_level="2"> + <maximum_takeoff_mass 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>1510141.8121567257</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>3738773.1116968105</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>5290910.387611725</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>15.378433652526235</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>-0.4654642512511066</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </center_of_gravity> + <mass description="Mass"> + <value>0</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>820612.3650779686</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>2031652.5381796542</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>2875085.274536487</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>15.108078043920829</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>-0.7480947757156718</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </center_of_gravity> + <mass description="Mass"> + <value>0</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>755918.7865518769</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>1871485.7181196488</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>2648425.8152194647</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>15.04983525477432</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>-0.8121168624538313</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </center_of_gravity> + <mass description="Mass"> + <value>39545.4300408</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>1189535.7164083032</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>2945024.179920398</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>4167639.640009298</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>15.6372561241248</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>-0.5909171268946131</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </center_of_gravity> + <mass description="Mass"> + <value>62229.835124</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + </mass_properties> + </maximum_zero_fuel_mass> + <maximum_payload_mass description=""> + <mass_properties description="maximum payload mass properties"> + <inertia description="Inertia with regard to the total center of gravity."> + <j_xx description="Inertia in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>16.8143301</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>19300.0</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>1273324.0627619973</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>3152465.3711376246</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>4461199.243825872</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>15.108078043920829</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>-0.7480947757156718</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </center_of_gravity> + <mass description="Mass"> + <value>66613.1713340691</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 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to the total center of gravity."> + <j_xx description="Inertia in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>15.556040431392383</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>-0.5318682062042068</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </center_of_gravity> + <mass description="Mass"> + <value>65786.26159731786</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>820612.3650779686</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + 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</j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>14.505998794238808</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>65462.14738244548</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>820612.3650779686</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>2031652.5381796542</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>2875085.274536487</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>15.764874650500401</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>67862.14738244549</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>1510141.8121567257</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>3738773.1116968105</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>5290910.387611725</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>15.378433652526235</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>-0.4654642512511066</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </center_of_gravity> + <mass description="Mass"> + <value>79002.14738244547</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + </mass_properties> + </design_mass> + <design_fuel_mass description=""> + <mass_properties description="design fuel mass properties"> + <inertia description="Inertia with regard to the total center of gravity."> + <j_xx description="Inertia in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity w.r.t global coordinate system."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>14.412288484467158</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>16992.947341067287</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-2020_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>35.45215648</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </b> + <MAC description="Mean aerodynamic chord"> + <value>4.159695001</value> + <unit>m</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </MAC> + <S_ref description="Wing reference area"> + <value>122.024796</value> + <unit>m^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </S_ref> + <neutral_point> + <x description="x component of neutral point"> + <value>16.54053159</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>0.549</value> + <unit>1</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </C_LoptimumCruise> + <C_LmaxLanding description="C_LmaxLanding"> + <value>2.135</value> + <unit>1</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </C_LmaxLanding> + <C_LmaxT-O description="C_LmaxTO"> + <value>1.981</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>4538397.521</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5000000</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>7.323960304e+11</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1e+12</upper_boundary> + </consumed_energy> + <energy_carrier_ID description="See energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </mission_energy> + </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>6.022727396e+11</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1e+12</upper_boundary> + </consumed_energy> + <energy_carrier_ID description="See energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </trip_energy> + <takeoff_energy ID="0" description="Amount of energy needed for takeoff segment for specified energy carrier"> + <consumed_energy description="Energy amount"> + <value>8371897678</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1e+12</upper_boundary> + </consumed_energy> + <energy_carrier_ID description="See energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </takeoff_energy> + <landing_energy ID="0" description="Amount of energy needed for landing segment for specified energy carrier"> + <consumed_energy description="Energy amount"> + <value>7153542456</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1e+12</upper_boundary> + </consumed_energy> + <energy_carrier_ID description="See energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </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>9509372061</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1e+12</upper_boundary> + </consumed_energy> + <energy_carrier_ID description="See energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </taxi_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>5282984478</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1e+12</upper_boundary> + </consumed_energy> + <energy_carrier_ID description="See energy carrier specification node"> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5</upper_boundary> + </energy_carrier_ID> + </taxi_in_energy> + </taxi_energy> + <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing"> + <value>21018.43583</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>20178.43583</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>0.5359768657</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>0.5119970814</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>0.5853999993</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>77169.13482</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>65413.90831</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>322125.6425</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>500000</upper_boundary> + </top_of_climb_range> + <top_of_descent_range description="Flown range from takeoff to top of descent"> + <value>4342074.947</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5000000</upper_boundary> + </top_of_descent_range> + <cruise_steps description="Cruise step information"> + <cruise_step ID="0" description="Data of a cruise step"> + <relative_end_of_cruise_step description="End of cruise step relative to total cruise length"> + <value>0.4991304067</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>10058.4002</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>10668.0002</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>15000</upper_boundary> + </altitude> + </cruise_step> + </cruise_steps> + </cruise> + </design_mission> + </mission> + </analysis> + <component_design> + <global_reference_point> + <reference_component description="Global reference point of aircraft geometry"> + <value>fuselage</value> + </reference_component> + <x description="X coordinate of the global reference point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </x> + <y description="Y coordinate of the global reference point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </y> + <z description="Z coordinate of the global reference point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </z> + </global_reference_point> + <wing> + <mass_properties description="mass_properties of component wing"> + <mass description="component mass"> + <value>8860.090873</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="component inertia referred to local center of gravity"> + <j_xx description="wing inertia in x"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xx> + <j_yy description="wing inertia in y"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yy> + <j_zz description="wing inertia in z"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zz> + <j_xy description="wing inertia in xy"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xy> + <j_xz description="wing inertia in xz"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xz> + <j_yx description="wing inertia in yx"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yx> + <j_yz description="wing inertia in yz"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yz> + <j_zx description="wing inertia in zx"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zx> + <j_zy description="wing inertia in zy"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="component center of gravity with respect to global coordinate system"> + <x description="x position of center of gravity"> + <value>15.72374237</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>-0.6303854434</value> + <unit>m</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </z> + </center_of_gravity> + </mass_properties> + <position description="position of wing"> + <x description="x position"> + <value>11.51890797</value> + <unit>1</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </x> + <y description="y position"> + <value>0</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </y> + <z description="z position"> + <value>-1.030445071</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </position> + <specific> + <geometry> + <aerodynamic_surface ID="0" description="main_wing"> + <name description="name of surface"> + <value>main_wing</value> + </name> + <position description="reference position in aircraft coordinates"> + <x description="x coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </x> + <y description="y coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </y> + <z description="z coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </position> + <parameters description="aerodynamic surface parameters"> + <direction description="unit vector according to aircraft coordinate system for direction applied at position"> + <x description="x direction of unit vector"> + <value>0</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </x> + <y description="y direction of unit vector"> + <value>-1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </y> + <z description="z direction of unit vector"> + <value>0</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </direction> + <symmetric description="symmetric to local x-z plane"> + <value>true</value> + </symmetric> + <sections description="sections"> + <section ID="0"> + <chord_origin description="origin of chord (local)"> + <x description="x coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </x> + <y description="y coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </y> + <z description="z coordinate of point"> + <value>-0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </chord_origin> + <chord_length description="chord length of the section"> + <value>6.122921737</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>6.122921737</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>2.206655466</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>0.2916723362</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>-5.317823472</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>4.090984901</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>0.9140197858</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>9.291499097</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>1.377253963</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>-17.72607824</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>1.040896695</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>0.5925187878</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>-0.1141636212</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>-0.1141636212</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>-0.2040818106</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.85</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.294</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + <deflection> + <full_negative_deflection description="full negative deflection"> + <value>0</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_negative_deflection> + <full_positive_deflection description="full positive deflection"> + <value>0.7853981634</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_positive_deflection> + </deflection> + </control_device> + <control_device ID="6" description="spoiler_air"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.85</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.306</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.85</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.4195</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + <deflection> + <full_negative_deflection description="full negative deflection"> + <value>0</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_negative_deflection> + <full_positive_deflection description="full positive deflection"> + <value>0.7853981634</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_positive_deflection> + </deflection> + </control_device> + <control_device ID="7" description="spoiler_air"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.85</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.4195</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.85</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.533</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + <deflection> + <full_negative_deflection description="full negative deflection"> + <value>0</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_negative_deflection> + <full_positive_deflection description="full positive deflection"> + <value>0.7853981634</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_positive_deflection> + </deflection> + </control_device> + <control_device ID="8" description="spoiler_air"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.85</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.533</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.85</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.6465</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + <deflection> + <full_negative_deflection description="full negative deflection"> + <value>0</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_negative_deflection> + <full_positive_deflection description="full positive deflection"> + <value>0.7853981634</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_positive_deflection> + </deflection> + </control_device> + <control_device ID="9" description="spoiler_air"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.85</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.6465</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.85</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.76</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + <deflection> + <full_negative_deflection description="full negative deflection"> + <value>0</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_negative_deflection> + <full_positive_deflection description="full positive deflection"> + <value>0.7853981634</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_positive_deflection> + </deflection> + </control_device> + </control_devices> + </parameters> + </aerodynamic_surface> + </geometry> + </specific> + </wing> + <empennage> + <position description="position of empennage"> + <x description="x position"> + <value>30.84621438</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>1284.974715</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="component inertia referred to local center of gravity"> + <j_xx description="Conventional tail overall mass inertia in x"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xx> + <j_yy description="Conventional tail overall mass inertia in y"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yy> + <j_zz description="Conventional tail overall mass inertia in z"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zz> + <j_xy description="Conventional tail overall mass inertia in xy"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xy> + <j_xz description="Conventional tail overall mass inertia in xz"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xz> + <j_yx description="Conventional tail overall mass inertia in yx"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yx> + <j_yz description="Conventional tail overall mass inertia in yz"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yz> + <j_zx description="Conventional tail overall mass inertia in zx"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zx> + <j_zy description="Conventional tail overall mass inertia in zy"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="component center of gravity with respect to global coordinate system"> + <x description="x position of center of gravity"> + <value>34.87847331</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>3.018558414</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"> + 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<lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </geometric_twist> + <scale_thickness description="scale the thickness defined by the profile with this factor"> + <value>1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </scale_thickness> + <profile description="profile (data normalized to chord length)"> + <value>n0012</value> + </profile> + </section> + <section ID="1"> + <chord_origin description="origin of chord (local)"> + <x description="x coordinate of point"> + <value>5.218300973</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 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<value>n0012</value> + </profile> + </section> + </sections> + <spars> + <spar ID="0" description="front_spar"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.2</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.2</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.2</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.2</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + </spar> + <spar ID="1" description="rear_spar"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.6</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.6</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.6</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.6</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + </spar> + </spars> + <control_devices> + <control_device ID="0" description="rudder"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.9</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + <deflection> + <full_negative_deflection description="full negative deflection"> + <value>-0.4363323125</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_negative_deflection> + <full_positive_deflection description="full positive deflection"> + <value>0.4363323125</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_positive_deflection> + </deflection> + </control_device> + </control_devices> + </parameters> + </aerodynamic_surface> + <aerodynamic_surface ID="1" description="horizontal_stabiliser"> + <name description="name of surface"> + <value>horizontal_stabiliser</value> + </name> + <position description="reference position in aircraft coordinates"> + <x description="x coordinate of point"> + <value>2.214733313</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>-0.5869147662</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>3.230234937</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>3.532093643</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>0.4945324201</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>-5.652531425</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>0.911572299</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </chord_length> + <geometric_twist description="geometric twist of the section around leading edge"> + <value>-0</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </geometric_twist> + <scale_thickness description="scale the thickness defined by the profile with this factor"> + <value>1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </scale_thickness> + <profile description="profile (data normalized to chord length)"> + <value>n0012</value> + </profile> + </section> + </sections> + <spars> + <spar ID="0" description="front_spar"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.2</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.2</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.2</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.2</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + </spar> + <spar ID="1" description="rear_spar"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.6</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.6</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.6</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>0.6</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + </spar> + </spars> + <control_devices> + <control_device ID="0" description="elevator"> + <position description="relative chord position"> + <inner_position description="relative inner position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.2</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </inner_position> + <outer_position description="relative outer position"> + <chord description="chord position"> + <from description="relative chord position"> + <value>0.7</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </from> + <to description="relative chord position"> + <value>1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </to> + </chord> + <spanwise description="relative spanwise position"> + <value>-0.9</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </spanwise> + </outer_position> + </position> + <deflection> + <full_negative_deflection description="full negative deflection"> + <value>-0.4363323125</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_negative_deflection> + <full_positive_deflection description="full positive deflection"> + <value>0.4363323125</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </full_positive_deflection> + </deflection> + </control_device> + </control_devices> + </parameters> + </aerodynamic_surface> + </geometry> + </specific> + </empennage> + <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>9227.545786</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>358507.5774</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>12053.92335</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>362014.3132</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>-0.04007228226</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>2014.79068</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>-0.04007228226</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>-0.003671168329</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>2014.79068</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>-0.003671168329</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>13.39098398</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>-2.45044457</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>2.251356929</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>2.251356929</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>0.858606747</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>2.814196161</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>2.814196161</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>2.575820241</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>2.814196161</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>2.814196161</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>3.434426988</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>2.251356929</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>2.251356929</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>1044.421165</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>52.54222833</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xx> + <j_yy description="inertia of the component"> + <value>53.71263772</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yy> + <j_zz description="inertia of the component"> + <value>53.71822863</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>-0.004167372537</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>0.004259196874</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>-0.004167372537</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>0.0005734046682</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>0.004259196874</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>0.0005734046682</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>13.23123029</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>-6.178624397</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>-2.633399725</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>-1.125678464</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </normal> + <sections description="sections"> + <section ID="0"> + <origin description="origin of chord (local)"> + <x description="x coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </x> + <y description="y coordinate of point"> + <value>1.378558528e-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>-1.125678464</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>3.434426988</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </chord_length> + <geometric_twist description="geometric twist of the section around leading edge"> + <value>-0</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </geometric_twist> + <profile description="profile (data normalized to chord length)"> + <value>pylon</value> + </profile> + </section> + <section ID="1"> + <origin description="origin of chord (local)"> + <x description="x coordinate of point"> + <value>2.703045251</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>2.412477425e-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>-1.969937313</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>3.434426988</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>545.3606608</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>0.6045290934</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>12.37643343</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>12.03331888</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>-0.01586876859</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xy> + <j_xz description="inertia of the component"> + <value>1.402798952</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>-0.01586876859</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>-0.00240898882</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yz> + <j_zx description="inertia of the component"> + <value>1.402798952</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>-0.00240898882</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system"> + <x description="x coordinate of the center of gravity"> + <value>14.58275291</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>-6.178624397</value> + <unit>m</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </y> + <z description="z coordinate of the center of gravity"> + <value>-1.085591836</value> + <unit>m</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </z> + </center_of_gravity> + </mass_properties> + </pylon> + <engine> + <model description="Name of selected engine model"> + <value>PW1127G-JM</value> + </model> + <position description="Position of the engine in the global coordinate system"> + <x description="x coordinate of point"> + <value>11.51401679</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>-6.178624397</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>-2.633399725</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>3023.991067</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>1915.928172</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>3930.368067</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>3930.368067</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>13.23123029</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>-6.178624397</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>-2.633399725</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>123410.9874</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>1.024752864</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>20359.19396</value> + <unit>N</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </thrust> + <tsfc description="Thrust specific fuel consumption of the engine at the bucket point"> + <value>1.505601144e-05</value> + <unit>kg/Ns</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </tsfc> + </bucket_point> + </engine> + </propulsion> + <propulsion ID="1" description="Description of one propulsion"> + <nacelle ID="0" description="Nacelle of the propulsion assembly"> + <position description="Origin of the nacelle RELATIVE to the engine position."> + <x description="x coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </x> + <y description="y coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </y> + <z description="z coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </position> + <normal description="Normal direction of the nacelle in the global aircraft coordinate system"> + <x description="x direction of unit vector"> + <value>1</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </x> + <y description="y direction of unit vector"> + <value>0</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </y> + <z description="z direction of unit vector"> + <value>0</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </normal> + <sections description="Geometrical description nacelle sections"> + <section ID="0"> + <origin description="Origin of the section (local)"> + <x description="x coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </x> + <y description="y coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </y> + <z description="z coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </origin> + <width description="width of the section"> + <value>2.251356929</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>2.251356929</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>0.858606747</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>2.814196161</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>2.814196161</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>2.575820241</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>2.814196161</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>2.814196161</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>3.434426988</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>2.251356929</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>2.251356929</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>1044.421165</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>52.54222833</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xx> + <j_yy description="inertia of the component"> + <value>53.71263772</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yy> + <j_zz description="inertia of the component"> + <value>53.71822863</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>-0.004167372537</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>0.004259196874</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>-0.004167372537</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>0.0005734046682</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>0.004259196874</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>0.0005734046682</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>13.23123029</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>6.178624397</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>-2.633399725</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>-1.125678464</value> + <unit>1</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </normal> + <sections description="sections"> + <section ID="0"> + <origin description="origin of chord (local)"> + <x description="x coordinate of point"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </x> + <y description="y coordinate of point"> + <value>1.378558528e-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>-1.125678464</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>3.434426988</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </chord_length> + <geometric_twist description="geometric twist of the section around leading edge"> + <value>-0</value> + <unit>rad</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </geometric_twist> + <profile description="profile (data normalized to chord length)"> + <value>pylon</value> + </profile> + </section> + <section ID="1"> + <origin description="origin of chord (local)"> + <x description="x coordinate of point"> + <value>2.703045251</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>2.412477425e-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>-1.969937313</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>3.434426988</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>545.3606608</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>0.6045290934</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>12.37643343</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>12.03331888</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>-0.01586876859</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xy> + <j_xz description="inertia of the component"> + <value>1.402798952</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>-0.01586876859</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>-0.00240898882</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yz> + <j_zx description="inertia of the component"> + <value>1.402798952</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>-0.00240898882</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system"> + <x description="x coordinate of the center of gravity"> + <value>14.58275291</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>6.178624397</value> + <unit>m</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </y> + <z description="z coordinate of the center of gravity"> + <value>-1.085591836</value> + <unit>m</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </z> + </center_of_gravity> + </mass_properties> + </pylon> + <engine> + <model description="Name of selected engine model"> + <value>PW1127G-JM</value> + </model> + <position description="Position of the engine in the global coordinate system"> + <x description="x coordinate of point"> + <value>11.51401679</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>6.178624397</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>-2.633399725</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>3023.991067</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>1915.928172</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>3930.368067</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>3930.368067</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>13.23123029</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>6.178624397</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>-2.633399725</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>123410.9874</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>1.024752864</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>20359.19396</value> + <unit>N</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </thrust> + <tsfc description="Thrust specific fuel consumption of the engine at the bucket point"> + <value>1.505601144e-05</value> + <unit>kg/Ns</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </tsfc> + </bucket_point> + </engine> + </propulsion> + </specific> + </propulsion> + <systems> + <mass_properties description="mass_properties of component systems"> + <mass description="component mass"> + <value>5446.81491</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </mass> + <inertia description="component inertia referred to local center of gravity"> + <j_xx description="systems inertia in x"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xx> + <j_yy description="systems inertia in y"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yy> + <j_zz description="systems inertia in z"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zz> + <j_xy description="systems inertia in xy"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xy> + <j_xz description="systems inertia in xz"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xz> + <j_yx description="systems inertia in yx"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yx> + <j_yz description="systems inertia in yz"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yz> + <j_zx description="systems inertia in zx"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zx> + <j_zy description="systems inertia in zy"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="component center of gravity with respect to global coordinate system"> + <x description="x position of center of gravity"> + <value>7.510092571</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>3.061460869</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </x> + <y description="y position of center of gravity"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </y> + <z description="z position of center of gravity"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </z> + </center_of_gravity> + </mass_properties> + </operator_item> + <operator_item ID="1"> + <name description="name of the operator item"> + <value>residual_oil_and_fuel</value> + </name> + <mass_properties description="mass_properties of component water and toilet chemicals"> + <mass description="component mass"> + <value>0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </mass> + <inertia description="component inertia referred to local center of gravity"> + <j_xx description="water and toilet chemicals inertia in x"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xx> + <j_yy description="water and toilet chemicals inertia in y"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yy> + <j_zz description="water and toilet chemicals inertia in z"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zz> + <j_xy description="water and toilet chemicals inertia in xy"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xy> + <j_xz description="water and toilet chemicals inertia in xz"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_xz> + <j_yx description="water and toilet chemicals inertia in yx"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yx> + <j_yz description="water and toilet chemicals inertia in yz"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_yz> + <j_zx description="water and toilet chemicals inertia in zx"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zx> + <j_zy description="water and toilet chemicals inertia in zy"> + <value>0</value> + <unit>kgm^2</unit> + <lower_boundary>-1.797693135e+308</lower_boundary> + <upper_boundary>1.797693135e+308</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="component center of gravity with respect to global coordinate system"> + <x description="x position of center of gravity"> + <value>15.72374237</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>260.2783506</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </fuel_system> + <de_icing description="mass of ATA-30"> + <value>38.20847961</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </de_icing> + <lighting description="mass of ATA-33"> + <value>232.9926862</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </lighting> + <fire_protection description="mass of ATA-26"> + <value>84.37707073</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </fire_protection> + <oxygen_system description="mass of ATA-35"> + <value>99.86208</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </oxygen_system> + <flight_controls description="mass of ATA-27"> + <value>1207.855649</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </flight_controls> + <instruments description="mass of ATA31"> + <value>76.35389846</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </instruments> + <automatic_flight_system description="mass of ATA22"> + <value>124.075085</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </automatic_flight_system> + <navigation description="mass of ATA34"> + <value>505.8445773</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </navigation> + <communication description="mass of ATA23"> + <value>248.15017</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </communication> + <bleed_air_system description="mass of ATA-36"> + <value>173.1963797</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>118.1462372</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </hydraulic_generation> + <hydraulic_distribution description="mass of ATA-29"> + <value>551.7045686</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </hydraulic_distribution> + <electrical_generation description="mass of ATA-24"> + <value>522.4924205</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </electrical_generation> + <electrical_distribution description="mass of ATA-24"> + <value>449.1695342</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>173.7035449</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>335.6041788</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>232657.9673</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>2.157080241</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>60778.51494</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>W</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>15542.96614</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="Inertia of all fuselages with regard to the total center of gravity."> + <j_xx description="Inertia of the of all fuselages in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of the of all fuselages in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of the of all fuselages in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of all fuselages in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of all fuselages in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of all fuselages in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of all fuselages in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of all fuselages in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of all fuselages in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of all fuselages."> + <x description="Center of gravity in x-direction with regard to the global reference point. (of all fuselages)"> + <value>16.8143301</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>50</upper_boundary> + </x> + <y description="Center of gravity in y-direction with regard to the global reference point. (of all fuselages)"> + <value>0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </y> + <z description="Center of gravity in z-direction with regard to the global reference point. (of all fuselages)"> + <value>-0.2413</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </center_of_gravity> + </mass_properties> + <specific description="Fuselage design specific output parameter."> + <geometry description="Geometry description of the entire fuselage design."> + <fuselage ID="0" description="Geometrical description of one entire fuselage."> + <name description="Name of the fuselage."> + <value>fuselage_0</value> + </name> + <position description="Position of one entire fuselage with regard to the fuselage global position."> + <x description="Distance in x direction with regard to the fuselage gear global position."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-100</lower_boundary> + <upper_boundary>100</upper_boundary> + </x> + <y description="Distance in y direction with regard to the fuselage gear global position."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-25</lower_boundary> + <upper_boundary>25</upper_boundary> + </y> + <z description="Distance in z direction with regard to the fuselage gear global position."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <direction description="Unit vector according to global coordinate system for direction applied at position."> + <x description="X component of the unit vector."> + <value>1</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </x> + <y description="Y component of the unit vector."> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </y> + <z description="Z component of the unit vector."> + <value>0</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </z> + </direction> + <mass_properties description="Mass properties of one entire fuselage."> + <mass description="Mass of one entire fuselage."> + <value>15542.966136707</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>0.267784187</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>0.496500597</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="1" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_1</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>0.467145347</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>0.836740921</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="2" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_2</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>0.617001451</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>1.09949371</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="3" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_3</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>0.811634047</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>1.332869486</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="4" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_4</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>0.976318453</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>1.597847703</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="5" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_5</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>1.21146329</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>1.950706682</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="6" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_6</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>1.429827854</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>2.243644807</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="7" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_7</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>1.867364888</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>2.796234326</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="8" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_8</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>1.971983901</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.095828445</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="9" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_9</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>2.113593806</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.508608277</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="10" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_10</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>2.167125385</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.762303773</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="11" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_11</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>2.219197163</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.908262138</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="12" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_12</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <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>2.227075627</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.967986828</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="13" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_13</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <x description="Distance in x direction with regard to the global reference point."> + <value>-0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </x> + <y description="Distance in y direction with regard to the global reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </y> + <z description="Distance in z direction with regard to the global reference point."> + <value>6.237748405</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </z> + </origin> + <upper_height description="Height of the upper half of the fuselage section."> + <value>1.915417119</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </upper_height> + <lower_height description="Height of the lower half of the fuselage section."> + <value>2.227075627</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.967986828</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="14" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_14</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <x description="Distance in x direction with regard to the global reference point."> + <value>-0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </x> + <y description="Distance in y direction with regard to the global reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </y> + <z description="Distance in z direction with regard to the global reference point."> + <value>27.5216784</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </z> + </origin> + <upper_height description="Height of the upper half of the fuselage section."> + <value>1.915413925</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </upper_height> + <lower_height description="Height of the lower half of the fuselage section."> + <value>2.227071912</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.967986828</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="15" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_15</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <x description="Distance in x direction with regard to the global reference point."> + <value>-0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </x> + <y description="Distance in y direction with regard to the global reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </y> + <z description="Distance in z direction with regard to the global reference point."> + <value>27.42759412</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </z> + </origin> + <upper_height description="Height of the upper half of the fuselage section."> + <value>1.915413925</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </upper_height> + <lower_height description="Height of the lower half of the fuselage section."> + <value>2.227071912</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.967986828</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="16" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_16</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <x description="Distance in x direction with regard to the global reference point."> + <value>-0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </x> + <y description="Distance in y direction with regard to the global reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </y> + <z description="Distance in z direction with regard to the global reference point."> + <value>31.85324279</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </z> + </origin> + <upper_height description="Height of the upper half of the fuselage section."> + <value>1.699062858</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </upper_height> + <lower_height description="Height of the lower half of the fuselage section."> + <value>1.736603193</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.3288491</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="17" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_17</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <x description="Distance in x direction with regard to the global reference point."> + <value>-0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </x> + <y description="Distance in y direction with regard to the global reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </y> + <z description="Distance in z direction with regard to the global reference point."> + <value>32.70160959</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </z> + </origin> + <upper_height description="Height of the upper half of the fuselage section."> + <value>1.657090968</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </upper_height> + <lower_height description="Height of the lower half of the fuselage section."> + <value>1.517243141</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>3.095828445</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="18" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_18</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <x description="Distance in x direction with regard to the global reference point."> + <value>-0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </x> + <y description="Distance in y direction with regard to the global reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </y> + <z description="Distance in z direction with regard to the global reference point."> + <value>34.3983432</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </z> + </origin> + <upper_height description="Height of the upper half of the fuselage section."> + <value>1.575335554</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </upper_height> + <lower_height description="Height of the lower half of the fuselage section."> + <value>0.939595006</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>2.46334671</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + <section ID="19" description="Geometrical description of one fuselage section."> + <name description="Name of the fuselage section."> + <value>section_19</value> + </name> + <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse."> + <value>ellipse</value> + </section_shape> + <origin description="Origin of fuselage section (local)."> + <x description="Distance in x direction with regard to the global reference point."> + <value>-0</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </x> + <y description="Distance in y direction with regard to the global reference point."> + <value>0.92429206</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </y> + <z description="Distance in z direction with regard to the global reference point."> + <value>37.35925828</value> + <unit>m</unit> + <lower_boundary>-75</lower_boundary> + <upper_boundary>75</upper_boundary> + </z> + </origin> + <upper_height description="Height of the upper half of the fuselage section."> + <value>0.528165979</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </upper_height> + <lower_height description="Height of the lower half of the fuselage section."> + <value>0.614104138</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </lower_height> + <width description="Width of the fuselage section."> + <value>0.559150813</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10</upper_boundary> + </width> + </section> + </sections> + <number_of_required_cabin_crew description="Number of minimum required flight attendants."> + <value>4</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100</upper_boundary> + </number_of_required_cabin_crew> + <mass_breakdown description="Mass breakdown of fuselage design module in accordance to CPACS."> + <fuselage_structure description="Mass breakdown of the fuselage structure block."> + <component_mass ID="0" description="Mass of a single component of the fuselage structure block."> + <name description="Name of the fuselage structure component."> + <value>door_mass</value> + </name> + <mass description="Mass of the fuselage structure component."> + <value>360.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100000</upper_boundary> + </mass> + </component_mass> + <component_mass ID="1" description="Mass of a single component of the fuselage structure block."> + <name description="Name of the fuselage structure component."> + <value>fuselage_mass</value> + </name> + <mass description="Mass of the fuselage structure component."> + <value>9049.071278727</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>619.536640625</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>319.955535336</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100000</upper_boundary> + </mass> + </component_mass> + <component_mass ID="12" description="Mass of a single component of the fuselage furnishing block."> + <name description="Name of the fuselage furnishing component."> + <value>cargo_loadings_mass</value> + </name> + <mass description="Mass of the fuselage furnishing component."> + <value>264.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100000</upper_boundary> + </mass> + </component_mass> + <component_mass ID="13" description="Mass of a single component of the fuselage furnishing block."> + <name description="Name of the fuselage furnishing component."> + <value>miscellaneous_mass</value> + </name> + <mass description="Mass of the fuselage furnishing component."> + <value>272.217252253</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>260.48508319999996</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100000</upper_boundary> + </mass> + </component_mass> + <component_mass ID="1" description="Mass of a single component of the fuselage operator items block."> + <name description="Name of the fuselage operator items component."> + <value>flight_attendant_mass</value> + </name> + <mass description="Mass of the fuselage operator item component."> + <value>280.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100000</upper_boundary> + </mass> + </component_mass> + <component_mass ID="2" description="Mass of a single component of the fuselage operator items block."> + <name description="Name of the fuselage operator items component."> + <value>in_flight_entertainment</value> + </name> + <mass description="Mass of the fuselage operator item component."> + <value>90.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100000</upper_boundary> + </mass> + </component_mass> + <component_mass ID="3" description="Mass of a single component of the fuselage operator items block."> + <name description="Name of the fuselage operator items component."> + <value>total_fixed_galley_mass</value> + </name> + <mass description="Mass of the fuselage operator item component."> + <value>315.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100000</upper_boundary> + </mass> + </component_mass> + <component_mass ID="4" description="Mass of a single component of the fuselage operator items block."> + <name description="Name of the fuselage operator items component."> + <value>total_seat_mass</value> + </name> + <mass description="Mass of the fuselage operator item component."> + <value>1242.0</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>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>6133.89485798</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>-2.089658</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>-2.089658</value> + <unit>m</unit> + <lower_boundary>-15</lower_boundary> + <upper_boundary>0</upper_boundary> + </lower_z> + </aft_reference_points> + </payload_tube_reference_points> + <payload_tube_wall_reference_points description="Payload tube wall reference points in x, y and z-direction referred to fuselage nose point."> + <front_reference_points description="Reference points in the front of payload tube."> + <x description="Wall reference point in x-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-100</lower_boundary> + <upper_boundary>100</upper_boundary> + </x> + <left_y description="Left wall reference point in y-direction."> + <value>-1.84658</value> + <unit>m</unit> + <lower_boundary>-35</lower_boundary> + <upper_boundary>35</upper_boundary> + </left_y> + <right_y description="Right wall reference point in y-direction."> + <value>1.84658</value> + <unit>m</unit> + <lower_boundary>-35</lower_boundary> + <upper_boundary>35</upper_boundary> + </right_y> + <z description="Wall reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-15</lower_boundary> + <upper_boundary>15</upper_boundary> + </z> + </front_reference_points> + <aft_reference_points description="Reference points in the aft of payload tube."> + <x description="Wall reference point in x-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-100</lower_boundary> + <upper_boundary>100</upper_boundary> + </x> + <left_y description="Left wall reference point in y-direction."> + <value>-1.84658</value> + <unit>m</unit> + <lower_boundary>-35</lower_boundary> + <upper_boundary>35</upper_boundary> + </left_y> + <right_y description="Right wall reference point in y-direction."> + <value>1.84658</value> + <unit>m</unit> + <lower_boundary>-35</lower_boundary> + <upper_boundary>35</upper_boundary> + </right_y> + <z description="Wall reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-15</lower_boundary> + <upper_boundary>15</upper_boundary> + </z> + </aft_reference_points> + </payload_tube_wall_reference_points> + <payload_tube_structural_wall_thickness description="Structural wall thickness of the payload tube."> + <value>0.137414</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </payload_tube_structural_wall_thickness> + <payload_tube_water_volume description="Total water volume of one entire payload tube."> + <value>188.925079455</value> + <unit>m^3</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1000</upper_boundary> + </payload_tube_water_volume> + <payload_decks description="Geometrical description of the payload decks."> + <payload_deck ID="0" description="Geometrical description of the payload decks in one payload tube."> + <name description="Name of the payload deck."> + <value>passenger_deck_1</value> + </name> + <position description="Position of the payload deck with regard to the payload tube reference point."> + <x description="Distance in x direction with regard to the payload tube reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-100</lower_boundary> + <upper_boundary>100</upper_boundary> + </x> + <y description="Distance in y direction with regard to the payload tube reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-0</lower_boundary> + <upper_boundary>0</upper_boundary> + </y> + <z description="Distance in z direction with regard to the payload tube reference point."> + <value>-0.4826</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck."> + <value>0.206248</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </payload_deck_structural_floor_thickness> + <payload_deck_water_volume description="Total water volume of the payload deck."> + <value>125.95005297</value> + <unit>m^3</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1000</upper_boundary> + </payload_deck_water_volume> + <payload_deck_length description="Total length of the payload deck."> + <value>27.016456</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100</upper_boundary> + </payload_deck_length> + <payload_deck_required_galley_power description="Required galley power of the payload deck."> + <value>9000</value> + <unit>W</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100000</upper_boundary> + </payload_deck_required_galley_power> + </payload_deck> + <payload_deck ID="1" description="Geometrical description of the payload decks in one payload tube."> + <name description="Name of the payload deck."> + <value>cargo_deck</value> + </name> + <position description="Position of the payload deck with regard to the payload tube reference point."> + <x description="Distance in x direction with regard to the payload tube reference point."> + <value>3.75</value> + <unit>m</unit> + <lower_boundary>-100</lower_boundary> + <upper_boundary>100</upper_boundary> + </x> + <y description="Distance in y direction with regard to the payload tube reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-0</lower_boundary> + <upper_boundary>0</upper_boundary> + </y> + <z description="Distance in z direction with regard to the payload tube reference point."> + <value>-1.831848</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck."> + <value>0.206248</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </payload_deck_structural_floor_thickness> + <payload_deck_water_volume description="Total water volume of the payload deck."> + <value>62.975026485</value> + <unit>m^3</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1000</upper_boundary> + </payload_deck_water_volume> + <payload_deck_length description="Total length of the payload deck."> + <value>13.508228</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100</upper_boundary> + </payload_deck_length> + <payload_deck_required_galley_power description="Required galley power of the payload deck."> + <value>0</value> + <unit>W</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>100000</upper_boundary> + </payload_deck_required_galley_power> + </payload_deck> + </payload_decks> + </payload_tube> + </fuselage_accommodation> + </fuselage> + </geometry> + </specific> + </fuselage> + <tank description="Description of aircraft tanks." tool_level="2"> + <position description="Tank reference point, position of the tanks with regard to the global reference point."> + <x description="Distance between the foremost tank end and the global reference point in x-direction."> + <value>11.51890797</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the foremost tank end and the global reference point in y-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the foremost middle tank end and the global reference point in z-direction."> + <value>-1.030445071</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <mass_properties description="Mass properties of all tanks."> + <mass description="Total tank mass."> + <value>0.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="Inertia of all tanks with regard to the total center of gravity."> + <j_xx description="Inertia of all tanks in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of all tanks in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of all tanks in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of all tanks in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of all tanks in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of all tanks in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of all tanks in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of all tanks in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of all tanks in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of all tanks."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Center of gravity in y-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Center of gravity in z-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </center_of_gravity> + </mass_properties> + <specific description="Tank design specific output parameter."> + <additional_fuselage_length description="Additional fuselage length (if smaller than 0: shrink fuselage, if greater than 0: stretch fuselage)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </additional_fuselage_length> + <tank ID="0" description="Description of one tank."> + <name description="Name of the tank."> + <value>tank_0</value> + </name> + <designator description="Designator of the tank."> + <value>wing_inner_left</value> + </designator> + <position description="Local reference point, position of one tank wrt. the tank reference point."> + <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction."> + <value>1.224584347</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction."> + <value>-1.983993414</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <direction description="Unit vector according to global coordinate system for direction applied at position."> + <x description="X component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </x> + <y description="Y component of the unit vector."> + <value>1</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </y> + <z description="Z component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </z> + </direction> + <mass_properties description="Mass properties of one tank."> + <mass description="Total dry mass of one tank."> + <value>0.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="Inertia of one tank with regard to its center of gravity."> + <j_xx description="Inertia of the of one tank in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of the of one tank in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of the of one tank in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of one tank in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of one tank in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of one tank in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of one tank in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of one tank in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of one tank in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of one tank."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Center of gravity in y-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Center of gravity in z-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </center_of_gravity> + <centroid description="Centroid of one tank."> + <x description="Centroid in x-direction with regard to the local reference point."> + <value>1.106851328</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Centroid in y-direction with regard to the local reference point."> + <value>-2.627613113</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>0.366654661</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>1.461678581e+11</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </maximum_energy_capacity> + <energy_capacity_required_for_mission description="Energy amount required for mission."> + <value>True</value> + </energy_capacity_required_for_mission> + <geometry description="Geometrical description of one tank."> + <cross_section ID="0" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_0</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the tank cross section and the local reference point in y-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.8265944344420982</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>2.4491686948</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + <cross_section ID="1" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_1</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>1.800268099</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>0.291672336</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>-3.333830058</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.5045956352728944</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.6363939604000004</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + </geometry> + </tank> + <tank ID="1" description="Description of one tank."> + <name description="Name of the tank."> + <value>tank_1</value> + </name> + <designator description="Designator of the tank."> + <value>wing_outer_left</value> + </designator> + <position description="Local reference point, position of one tank wrt. the tank reference point."> + <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction."> + <value>3.024852446</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction."> + <value>-5.317823472</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>0.291672336</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <direction description="Unit vector according to global coordinate system for direction applied at position."> + <x description="X component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </x> + <y description="Y component of the unit vector."> + <value>1</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </y> + <z description="Z component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </z> + </direction> + <mass_properties description="Mass properties of one tank."> + <mass description="Total dry mass of one tank."> + <value>0.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="Inertia of one tank with regard to its center of gravity."> + <j_xx description="Inertia of the of one tank in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of the of one tank in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of the of one tank in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of one tank in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of one tank in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of one tank in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of one tank in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of one tank in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of one tank in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of one tank."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Center of gravity in y-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Center of gravity in z-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </center_of_gravity> + <centroid description="Centroid of one tank."> + <x description="Centroid in x-direction with regard to the local reference point."> + <value>0.751239882</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Centroid in y-direction with regard to the local reference point."> + <value>-6.934994391</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>0.229172626</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>1.355603786e+11</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </maximum_energy_capacity> + <energy_capacity_required_for_mission description="Energy amount required for mission."> + <value>True</value> + </energy_capacity_required_for_mission> + <geometry description="Geometrical description of one tank."> + <cross_section ID="0" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_0</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the tank cross section and the local reference point in y-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.5045956352728944</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.6363939604000004</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + <cross_section ID="1" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_1</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>4.742640471</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>1.057589192</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>-9.092176528</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.19595492134103498</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>0.7427500670062859</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + </geometry> + </tank> + <tank ID="2" description="Description of one tank."> + <name description="Name of the tank."> + <value>tank_2</value> + </name> + <designator description="Designator of the tank."> + <value>wing_inner_right</value> + </designator> + <position description="Local reference point, position of one tank wrt. the tank reference point."> + <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction."> + <value>1.224584347</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction."> + <value>1.983993414</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <direction description="Unit vector according to global coordinate system for direction applied at position."> + <x description="X component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </x> + <y description="Y component of the unit vector."> + <value>1</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </y> + <z description="Z component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </z> + </direction> + <mass_properties description="Mass properties of one tank."> + <mass description="Total dry mass of one tank."> + <value>0.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="Inertia of one tank with regard to its center of gravity."> + <j_xx description="Inertia of the of one tank in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of the of one tank in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of the of one tank in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of one tank in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of one tank in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of one tank in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of one tank in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of one tank in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of one tank in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of one tank."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Center of gravity in y-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Center of gravity in z-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </center_of_gravity> + <centroid description="Centroid of one tank."> + <x description="Centroid in x-direction with regard to the local reference point."> + <value>1.106851328</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Centroid in y-direction with regard to the local reference point."> + <value>2.627613113</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>0.366654661</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>1.461678581e+11</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </maximum_energy_capacity> + <energy_capacity_required_for_mission description="Energy amount required for mission."> + <value>True</value> + </energy_capacity_required_for_mission> + <geometry description="Geometrical description of one tank."> + <cross_section ID="0" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_0</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the tank cross section and the local reference point in y-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.8265944344420982</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>2.4491686948</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + <cross_section ID="1" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_1</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>1.800268099</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>0.291672336</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>3.333830058</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.5045956352728944</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.6363939604000004</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + </geometry> + </tank> + <tank ID="3" description="Description of one tank."> + <name description="Name of the tank."> + <value>tank_3</value> + </name> + <designator description="Designator of the tank."> + <value>wing_outer_right</value> + </designator> + <position description="Local reference point, position of one tank wrt. the tank reference point."> + <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction."> + <value>3.024852446</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction."> + <value>5.317823472</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>0.291672336</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <direction description="Unit vector according to global coordinate system for direction applied at position."> + <x description="X component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </x> + <y description="Y component of the unit vector."> + <value>1</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </y> + <z description="Z component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </z> + </direction> + <mass_properties description="Mass properties of one tank."> + <mass description="Total dry mass of one tank."> + <value>0.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="Inertia of one tank with regard to its center of gravity."> + <j_xx description="Inertia of the of one tank in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of the of one tank in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of the of one tank in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of one tank in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of one tank in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of one tank in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of one tank in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of one tank in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of one tank in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of one tank."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Center of gravity in y-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Center of gravity in z-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </center_of_gravity> + <centroid description="Centroid of one tank."> + <x description="Centroid in x-direction with regard to the local reference point."> + <value>0.751239882</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Centroid in y-direction with regard to the local reference point."> + <value>6.934994391</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>0.229172626</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>1.355603786e+11</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </maximum_energy_capacity> + <energy_capacity_required_for_mission description="Energy amount required for mission."> + <value>True</value> + </energy_capacity_required_for_mission> + <geometry description="Geometrical description of one tank."> + <cross_section ID="0" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_0</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the tank cross section and the local reference point in y-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.5045956352728944</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.6363939604000004</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + <cross_section ID="1" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_1</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>4.742640471</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>1.057589192</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>9.092176528</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.19595492134103498</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>0.7427500670062859</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + </geometry> + </tank> + <tank ID="4" description="Description of one tank."> + <name description="Name of the tank."> + <value>tank_4</value> + </name> + <designator description="Designator of the tank."> + <value>wing_center</value> + </designator> + <position description="Local reference point, position of one tank wrt. the tank reference point."> + <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction."> + <value>1.224584347</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <direction description="Unit vector according to global coordinate system for direction applied at position."> + <x description="X component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </x> + <y description="Y component of the unit vector."> + <value>1</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </y> + <z description="Z component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </z> + </direction> + <mass_properties description="Mass properties of one tank."> + <mass description="Total dry mass of one tank."> + <value>0.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="Inertia of one tank with regard to its center of gravity."> + <j_xx description="Inertia of the of one tank in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of the of one tank in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of the of one tank in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of one tank in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of one tank in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of one tank in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of one tank in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of one tank in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of one tank in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of one tank."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Center of gravity in y-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Center of gravity in z-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </center_of_gravity> + <centroid description="Centroid of one tank."> + <x description="Centroid in x-direction with regard to the local reference point."> + <value>1.224584347</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Centroid in y-direction with regard to the local reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Centroid in z-direction with regard to the local reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </centroid> + </mass_properties> + <maximum_energy_capacity description="Maximum energy capacity of one tank."> + <value>2.437021622e+11</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </maximum_energy_capacity> + <energy_capacity_required_for_mission description="Energy amount required for mission."> + <value>True</value> + </energy_capacity_required_for_mission> + <geometry description="Geometrical description of one tank."> + <cross_section ID="0" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_0</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the tank cross section and the local reference point in y-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>0.98207674</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.8265944344420982</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>2.4491686948</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + <cross_section ID="1" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_1</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the tank cross section and the local reference point in y-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>-0.98207674</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.8265944344420982</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>2.4491686948</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + </geometry> + </tank> + <tank ID="5" description="Description of one tank."> + <name description="Name of the tank."> + <value>tank_5</value> + </name> + <designator description="Designator of the tank."> + <value>fuselage_center</value> + </designator> + <position description="Local reference point, position of one tank wrt. the tank reference point."> + <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction."> + <value>6.222921737</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>-0.234554929</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <direction description="Unit vector according to global coordinate system for direction applied at position."> + <x description="X component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </x> + <y description="Y component of the unit vector."> + <value>1</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </y> + <z description="Z component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </z> + </direction> + <mass_properties description="Mass properties of one tank."> + <mass description="Total dry mass of one tank."> + <value>300</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="Inertia of one tank with regard to its center of gravity."> + <j_xx description="Inertia of the of one tank in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of the of one tank in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of the of one tank in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of one tank in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of one tank in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of one tank in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of one tank in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of one tank in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of one tank in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of one tank."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>7.002921737</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>-1.2488340970274752</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </center_of_gravity> + <centroid description="Centroid of one tank."> + <x description="Centroid in x-direction with regard to the local reference point."> + <value>0.78</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Centroid in y-direction with regard to the local reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Centroid in z-direction with regard to the local reference point."> + <value>-1.248834097</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>9.91892625e+10</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </maximum_energy_capacity> + <energy_capacity_required_for_mission description="Energy amount required for mission."> + <value>False</value> + </energy_capacity_required_for_mission> + <geometry description="Geometrical description of one tank."> + <cross_section ID="0" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_0</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>6.222921737</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>-0.007054929</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>1.22</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.695</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.56</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + <cross_section ID="1" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_1</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>6.222921737</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>-0.234554929</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>0.765</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>1.15</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.56</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>tank_section_2</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>6.222921737</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>-0.234554929</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>1.15</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.56</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>tank_section_3</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>6.222921737</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>-0.234554929</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>-0.765</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>1.15</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.56</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="4" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_4</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>6.222921737</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>-0.007054929</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>-1.22</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.695</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.56</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + </geometry> + </tank> + <tank ID="6" description="Description of one tank."> + <name description="Name of the tank."> + <value>tank_6</value> + </name> + <designator description="Designator of the tank."> + <value>horizontal_stabilizer_total</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>22.18808671</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>1.367822365</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <direction description="Unit vector according to global coordinate system for direction applied at position."> + <x description="X component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </x> + <y description="Y component of the unit vector."> + <value>1</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </y> + <z description="Z component of the unit vector."> + <value>0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </z> + </direction> + <mass_properties description="Mass properties of one tank."> + <mass description="Total dry mass of one tank."> + <value>0.0</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </mass> + <inertia description="Inertia of one tank with regard to its center of gravity."> + <j_xx description="Inertia of the of one tank in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of the of one tank in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of the of one tank in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of one tank in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of one tank in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of one tank in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of one tank in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of one tank in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of one tank in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of one tank."> + <x description="Center of gravity in x-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Center of gravity in y-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Center of gravity in z-direction with regard to the global reference point."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </center_of_gravity> + <centroid description="Centroid of one tank."> + <x description="Centroid in x-direction with regard to the local reference point."> + <value>0.78</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Centroid in y-direction with regard to the local reference point."> + <value>0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Centroid in z-direction with regard to the local reference point."> + <value>0.575</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>7.87640829e+10</value> + <unit>J</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </maximum_energy_capacity> + <energy_capacity_required_for_mission description="Energy amount required for mission."> + <value>False</value> + </energy_capacity_required_for_mission> + <geometry description="Geometrical description of one tank."> + <cross_section ID="0" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_0</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>0.711215719</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>0.010503343</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>5.539480797</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.34146778173167264</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.2723956019461944</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + <cross_section ID="1" description="Geometrical description of one tank cross section."> + <name description="Name of tank cross section."> + <value>tank_section_1</value> + </name> + <position description="Position of tank cross section with regard to the local reference point."> + <x description="Distance between the tank cross section and the local reference point in x-direction."> + <value>0.646046987</value> + <unit>m</unit> + <lower_boundary>-80</lower_boundary> + <upper_boundary>80</upper_boundary> + </x> + <y description="Distance between the tank cross section and the local reference point in y-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.3467541562458756</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.2920939747999998</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>tank_section_2</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>0.711215719</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>0.010503343</value> + <unit>m</unit> + <lower_boundary>-40</lower_boundary> + <upper_boundary>40</upper_boundary> + </y> + <z description="Distance between the tank cross section and the local reference point in z-direction."> + <value>-5.539480797</value> + <unit>m</unit> + <lower_boundary>-5</lower_boundary> + <upper_boundary>5</upper_boundary> + </z> + </position> + <shape description="Description of the shape of the cross section (circular, rectangular, elliptical)."> + <value>rectangular</value> + </shape> + <height description="Height of the cross section."> + <value>0.34146778173167264</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </height> + <width description="Width of the cross section."> + <value>1.2723956019461944</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </width> + <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap)."> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </length> + </cross_section> + </geometry> + </tank> + </specific> + </tank> + <landing_gear description="Geometric description of the aircraft undercarriage." tool_level="3"> + <position description="Position of the total undercarriage arrangement with regard to the global reference point."> + <x description="Distance in x direction with regard to the global reference point. (total undercarriage arrangement)"> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-100</lower_boundary> + <upper_boundary>100</upper_boundary> + </x> + <y description="Distance in y direction with regard to the global reference point. (total undercarriage arrangement)"> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-25</lower_boundary> + <upper_boundary>25</upper_boundary> + </y> + <z description="Distance in z direction with regard to the global reference point. (total undercarriage arrangement)"> + <value>0.0</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </position> + <mass_properties description="Mass properties of the total undercarriage arrangement."> + <mass description="Mass of the total undercarriage arrangement."> + <value>2567.3427</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>15.0496</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>-1.5763</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>[54.8, 49.0, 44.6, 42.7]</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>6.2</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>-1.4712</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </position> + <mass_properties description="Mass properties of one entire landing gear leg."> + <mass description="Mass of one entire landing gear leg."> + <value>383.0185</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>-9.2172</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>0.1051</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>0.7352</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>-0.7352</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>-0.7352</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>16.6658</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>2.8704</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>-0.953</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>1092.1621</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10000</upper_boundary> + </mass> + <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity."> + <j_xx description="Inertia of one entire landing gear leg in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of one entire landing gear leg in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of one entire landing gear leg in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of one entire landing gear leg in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of one entire landing gear leg in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of one entire landing gear leg in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of one entire landing gear leg in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of one entire landing gear leg in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of one entire landing gear leg in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of one entire landing gear leg."> + <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)"> + <value>0.9895</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>2.8704</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>0.2566</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </center_of_gravity> + </mass_properties> + <assembly_components description="Geometrical description of the assembly components of one landing gear strut."> + <strut_diameter description="Diameter of the landing gear strut"> + <value>0.2322</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.0</upper_boundary> + </strut_diameter> + <strut_length description="Length of the landing gear strut"> + <value>1.2534</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>-1.2534</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>-1.2534</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </position> + <tire_diameter description="Diameter of one tire of the wheel group."> + <value>1.1493</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>2</upper_boundary> + </tire_diameter> + <tire_section_width description="Width at the shoulder of a tire of the wheel group."> + <value>0.4064</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </tire_section_width> + </tire_description> + </assembly_components> + </landing_gear_assembly> + <landing_gear_assembly ID="2" description="Geometrical description of one entire landing gear leg."> + <name description="Name of the landing gear leg."> + <value>left_main_gear_outer_strut</value> + </name> + <position description="Position of one entire landing gear leg with regard to the landing gear global position."> + <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)"> + <value>16.6658</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>-2.8704</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>-0.953</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>1092.1621</value> + <unit>kg</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>10000</upper_boundary> + </mass> + <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity."> + <j_xx description="Inertia of one entire landing gear leg in x."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xx> + <j_yy description="Inertia of one entire landing gear leg in y."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yy> + <j_zz description="Inertia of one entire landing gear leg in z."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zz> + <j_xy description="Inertia of one entire landing gear leg in xy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xy> + <j_xz description="Inertia of one entire landing gear leg in xz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_xz> + <j_yx description="Inertia of one entire landing gear leg in yx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yx> + <j_yz description="Inertia of one entire landing gear leg in yz."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_yz> + <j_zx description="Inertia of one entire landing gear leg in zx."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zx> + <j_zy description="Inertia of one entire landing gear leg in zy."> + <value>0.0</value> + <unit>kgm^2</unit> + <lower_boundary>-inf</lower_boundary> + <upper_boundary>inf</upper_boundary> + </j_zy> + </inertia> + <center_of_gravity description="Center of gravity of one entire landing gear leg."> + <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)"> + <value>0.9895</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>2.8704</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>0.2566</value> + <unit>m</unit> + <lower_boundary>-10</lower_boundary> + <upper_boundary>10</upper_boundary> + </z> + </center_of_gravity> + </mass_properties> + <assembly_components description="Geometrical description of the assembly components of one landing gear strut."> + <strut_diameter description="Diameter of the landing gear strut"> + <value>0.2322</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1.0</upper_boundary> + </strut_diameter> + <strut_length description="Length of the landing gear strut"> + <value>1.2534</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>-1.2534</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>-1.2534</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>0.3185737265</value> + <unit>1</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>1</upper_boundary> + </thrust_to_weight> + <wing_loading description="Maximum takeoff mass (MTOM) divided by wing area (Sref)"> + <value>647.4483091</value> + <unit>kg/m^2</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>inf</upper_boundary> + </wing_loading> + </sizing_point> + <assessment description="Assessment data"> + <performance description="Assessment of performance values"> + <takeoff 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>1552.301412</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5000</upper_boundary> + </takeoff_distance_normal_safety> + </takeoff> + <landing description="Landing assessment"> + <needed_runway_length description="Needed runway length with all engines operating and maximum landing mass"> + <value>1288.31792</value> + <unit>m</unit> + <lower_boundary>0</lower_boundary> + <upper_boundary>5000</upper_boundary> + </needed_runway_length> + </landing> + </performance> + </assessment> +</aircraft_exchange_file> diff --git a/projects/oldFormat-CSR.xml b/projects/oldFormat-CSR.xml new file mode 100644 index 0000000000000000000000000000000000000000..6b4c8683fbe9007cce157f079ec5ee5b10ec17e7 --- /dev/null +++ b/projects/oldFormat-CSR.xml @@ -0,0 +1,3866 @@ +<AcftExchangeFile> + <General Desc="Allgemeine Angaben"> + <Type Desc="Flugzeugtyp" Unit="-">CeRAS</Type> + <Model Desc="Modell bzw. Ausfuehrung" Unit="-">CSR-01</Model> + </General> + <MassesAndLoadings Desc="-"> + <MassBreakdown Desc="Massenverteilung"> + <Wing Desc="Fluegelmasse und Schwerpunktlage des Massenelements, Airbus Chapter 10"> + <Mass ToolLevel="1" Unit="kg">8535.455741</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item> + <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item> + </RefPoint> + <CenterWing Desc="Masse der Fluegelstruktur (Skins, Spars, Ribs, Pylon attachments, LG supports), Airbus Ch. 10.0-4"> + <Mass ToolLevel="1" Unit="kg">6278.799947</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item> + <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item> + </RefPoint> + <EoW_CenterWingMassFactor Desc="Center wing mass factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_CenterWingMassFactor> + <EoW_AeroelasticFactor Desc="Aeroelastic (flutter) factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_AeroelasticFactor> + <EoW_TotalCenterWingMassFactor Desc="EoW_CenterWingMassFactor * EoW_AeroelasticFactor" ToolLevel="1" Unit="-">1</EoW_TotalCenterWingMassFactor> + </CenterWing> + <WingLEandTE Desc="Masse der Hochauftriebssysteme, Airbus Ch. 10.5-8"> + <Mass ToolLevel="1" Unit="kg">2256.655794</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item> + <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item> + </RefPoint> + <FixedLeadingEdge Desc="Mass of the complete fixed leading edge, Airbus Ch. 10.5"> + <Mass ToolLevel="1" Unit="kg">291.6450898</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item> + <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item> + </RefPoint> + </FixedLeadingEdge> + <MovableLeadingEdge Desc="Mass of the complete movable leading edge, Airbus Ch. 10.6"> + <Mass ToolLevel="1" Unit="kg">373.9546469</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item> + <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item> + </RefPoint> + </MovableLeadingEdge> + <FixedTrailingEdge Desc="Mass of the fixed trailing edge, Airbus Ch. 10.7"> + <Mass ToolLevel="1" Unit="kg">582.2672595</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item> + <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item> + </RefPoint> + </FixedTrailingEdge> + <MovableTrailingEdge Desc="Mass of the movable trailing edge, Airbus Ch. 10.8"> + <Mass ToolLevel="1" Unit="kg">1008.788798</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item> + <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item> + </RefPoint> + </MovableTrailingEdge> + </WingLEandTE> + <Miscellaneous Desc="Restliche Fluegelmassenanteile, Airbus Ch. 10.9"> + <Mass ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item> + <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item> + </RefPoint> + </Miscellaneous> + </Wing> + <Fuselage Desc="Rumpfmasse und Schwerpunktlage des Massenelements, Airbus Chapter 11"> + <Mass Desc="-" ToolLevel="1" Unit="kg">8888.102165</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Fuselage> + <Empennage Desc="Masse der Leitwerksgruppe und Schwerpunktlage des Massenelements"> + <Mass Desc="Gesamtmasse der Leitwerksgruppe" ToolLevel="1" Unit="kg">1257.118042</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.40806564</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item> + </RefPoint> + <Tailplane Desc="Airbus Chapter 13"> + <Mass ToolLevel="1" Unit="kg">705.5278242</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.73963722</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item> + </RefPoint> + </Tailplane> + <Fin Desc="Airbus Chapter 14"> + <Mass Desc="-" ToolLevel="1" Unit="kg">551.5902181</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">32.98395918</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item> + </RefPoint> + </Fin> + </Empennage> + <LandingGear Desc="Fahrwerksmasse und Schwerpunktlage des Massenelements, Airbus Chapter 15"> + <Mass Desc="-" ToolLevel="1" Unit="kg">2518.773274</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.32982807</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.469648031</h_Item> + </RefPoint> + <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear"> + <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">377.8159911</TotalMass> + <RefPoint Desc="Position of NoseGear CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + <Strut> + <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass> + <RefPoint Desc="position of strut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Strut> + <SupportStrut> + <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass> + <RefPoint Desc="position of suppStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </SupportStrut> + <WheelGroupConnection> + <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass> + <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </WheelGroupConnection> + <WheelGroup> + <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass> + <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass> + <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass> + <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass> + </WheelGroup> + </Gear> + <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear"> + <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1070.478642</TotalMass> + <RefPoint Desc="Position of OuterRightMainGear CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + <Strut> + <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass> + <RefPoint Desc="position of strut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Strut> + <SupportStrut> + <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass> + <RefPoint Desc="position of suppStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </SupportStrut> + <WheelGroupConnection> + <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass> + <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </WheelGroupConnection> + <WheelGroup> + <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass> + <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass> + <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass> + <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass> + </WheelGroup> + </Gear> + <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear"> + <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1070.478642</TotalMass> + <RefPoint Desc="Position of OuterLeftMainGear CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + <Strut> + <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass> + <RefPoint Desc="position of strut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Strut> + <SupportStrut> + <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass> + <RefPoint Desc="position of suppStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </SupportStrut> + <WheelGroupConnection> + <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass> + <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </WheelGroupConnection> + <WheelGroup> + <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass> + <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass> + <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass> + <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass> + </WheelGroup> + </Gear> + <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear"> + <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</TotalMass> + <RefPoint Desc="Position of InnerRightMainGear CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + <Strut> + <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass> + <RefPoint Desc="position of strut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Strut> + <SupportStrut> + <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass> + <RefPoint Desc="position of suppStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </SupportStrut> + <WheelGroupConnection> + <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass> + <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </WheelGroupConnection> + <WheelGroup> + <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass> + <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass> + <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass> + <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass> + </WheelGroup> + </Gear> + <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear"> + <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</TotalMass> + <RefPoint Desc="Position of InnerLeftMainGear CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + <Strut> + <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass> + <RefPoint Desc="position of strut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Strut> + <SupportStrut> + <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass> + <RefPoint Desc="position of suppStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </SupportStrut> + <WheelGroupConnection> + <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass> + <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference"> + <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </WheelGroupConnection> + <WheelGroup> + <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass> + <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass> + <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass> + <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass> + </WheelGroup> + </Gear> + </LandingGear> + <Pylons Desc="Pylonmasse und Schwerpunktlage (aller Pylons), Airbus Chapter 16"> + <Mass Desc="-" ToolLevel="1" Unit="kg">1049.543431</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.59758377</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.838904205</h_Item> + </RefPoint> + </Pylons> + <PowerUnit Desc="Masse und Schwerpunktlage der Triebwerksanlage, Airbus Group Power Unit"> + <Mass Desc="Gesamtmasse der Gruppe Antriebsanlage" ToolLevel="1" Unit="kg">7983.304178</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.56488425</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item 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Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item> + </RefPoint> + </EngineDry> + <Nacelle Desc="Nacelle mass"> + <Mass Desc="-" ToolLevel="1" Unit="kg">1069.077788</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item> + </RefPoint> + </Nacelle> + <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc."> + <Mass Desc="-" ToolLevel="1" Unit="kg">443.0846426</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item> + </RefPoint> + </OtherSystems> + <Prop Desc="Propeller mass"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Prop> + </Engine> + <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="2"> + <Mass Desc="-" ToolLevel="1" Unit="kg">3749.798796</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item> + </RefPoint> + <EngineDry Desc="Engine dry mass"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item> + </RefPoint> + </EngineDry> + <Nacelle Desc="Nacelle mass"> + <Mass Desc="-" ToolLevel="1" Unit="kg">1069.077788</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item> + </RefPoint> + </Nacelle> + <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc."> + <Mass Desc="-" ToolLevel="1" Unit="kg">443.0846426</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item> + </RefPoint> + </OtherSystems> + <Prop Desc="Propeller mass"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Prop> + </Engine> + <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="3"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + <EngineDry Desc="Engine dry mass"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </EngineDry> + <Nacelle Desc="Nacelle mass"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Nacelle> + <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc."> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </OtherSystems> + <Prop Desc="Propeller mass"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Prop> + </Engine> + <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="4"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + <EngineDry Desc="Engine dry mass"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global 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Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item> + </RefPoint> + </BleedAirSystem> + <EngineControls Desc="Airbus Chapter 22"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </EngineControls> + <FuelSystem Desc="Airbus Chapter 25, ATA28"> + <Mass Desc="-" ToolLevel="1" Unit="kg">313.2402355</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item> + <y_Item Desc="Position of reference in 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Unit="m">35.12321805</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </APU> + <HydraulicGeneration Desc="Airbus Chapter 31, ATA 29"> + <Mass Desc="-" ToolLevel="1" Unit="kg">177.4943728</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item> + </RefPoint> + </HydraulicGeneration> + <HydraulicDistribution Desc="Airbus Chapter 32, ATA 29"> + <Mass Desc="-" ToolLevel="1" Unit="kg">795.934215</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item> + </RefPoint> + </HydraulicDistribution> + <AirConditioning Desc="Airbus Chapter 33, ATA21"> + <Mass Desc="-" ToolLevel="1" Unit="kg">711.2165166</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item> + </RefPoint> + </AirConditioning> + <DeIcing Desc="Airbus Chapter 34, ATA30"> + <Mass Desc="-" ToolLevel="1" Unit="kg">41.98276817</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </DeIcing> + <FireProtection Desc="Airbus Chapter 35, ATA26"> + <Mass Desc="-" ToolLevel="1" Unit="kg">92.36094204</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </FireProtection> + <FlightControls Desc="Airbus Chapter 36, ATA27"> + <Mass Desc="-" ToolLevel="1" Unit="kg">699.137886</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item> + </RefPoint> + <Roll Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.0"> + <Mass Desc="-" ToolLevel="1" Unit="kg">42.43977661</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Roll> + <Yaw Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.1"> + <Mass Desc="-" ToolLevel="1" Unit="kg">97.75474213</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Yaw> + <Pitch Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.2"> + <Mass Desc="-" ToolLevel="1" Unit="kg">30.4466164</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Pitch> + <MovableHorizontalTail Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.3"> + <Mass Desc="-" ToolLevel="1" Unit="kg">63.38988998</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </MovableHorizontalTail> + <Flaps Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.4"> + <Mass Desc="-" ToolLevel="1" Unit="kg">143.8595475</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Flaps> + <SpoilersAirbrakesLiftdumpers Desc="Mass of the aileron actuators, their installations and 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</Slats> + <CommonInstallation Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.7"> + <Mass Desc="-" ToolLevel="1" Unit="kg">139.8275772</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </CommonInstallation> + </FlightControls> + <Instruments Desc="Airbus Chapter 37, ATA31"> + <Mass ToolLevel="1" Unit="kg">85.16128872</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">4.34075992</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Instruments> + <AutomaticFlightSystem Desc="Airbus Chapter 38, ATA 22"> + <Mass ToolLevel="1" Unit="kg">138.3870942</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </AutomaticFlightSystem> + <Navigation Desc="Airbus Chapter 39, ATA34"> + <Mass Desc="-" ToolLevel="1" Unit="kg">564.1935378</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Navigation> + <Communication Desc="Airbus Chapter 40, ATA23"> + <Mass Desc="-" ToolLevel="1" Unit="kg">276.7741884</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Communication> + <ElectricalGeneration Desc="Airbus Chapter 41, ATA24"> + <Mass Desc="-" ToolLevel="1" Unit="kg">774.2507101</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </ElectricalGeneration> + <ElectricalDistribution Desc="Airbus Chapter 42, ATA24"> + <Mass Desc="-" ToolLevel="1" Unit="kg">682.914046</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </ElectricalDistribution> + </Systems> + <Furnishings Desc="Furnishingmasse und Schwerpunktlage des Massenelements, Airbus Group Furnishings"> + <Mass Desc="Gesamtmasse der Furnishinggruppe" ToolLevel="1" Unit="kg">3114.623325</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + <Furnishing Desc="Airbus Chapter 50, ATA25"> + <Mass Desc="-" ToolLevel="1" Unit="kg">2464.223172</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Furnishing> + <FixedEmergencyOxygen Desc="Airbus Chapter 51, ATA35"> + <Mass Desc="-" ToolLevel="1" Unit="kg">98.464</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </FixedEmergencyOxygen> + <Lighting Desc="Airbus Chapter 52, ATA33"> + <Mass Desc="-" ToolLevel="1" Unit="kg">261.9261532</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </Lighting> + <WaterInstallation Desc="Airbus Chapter 53, ATA38"> + <Mass Desc="-" ToolLevel="1" Unit="kg">290.01</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </WaterInstallation> + </Furnishings> + <OperatorsItems Desc="Masse der Betreiberausstattung und Schwerpunktlage des Massenelements, Airbus Group Operator Items"> + <Mass Desc="Gesamtmasse der Operators Items Gruppe" ToolLevel="1" Unit="kg">3326.415065</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.54754916</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + <OperatorEquipment Desc="Airbus Chapter 60 (fixed equipment, vorher Standard Items)"> + <Mass Desc="-" ToolLevel="1" Unit="kg">1575.865065</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.5703719</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </OperatorEquipment> + <OperationalEquipment Desc="Airbus Chapter 61 (movable equipment)"> + <Mass Desc="-" ToolLevel="1" Unit="kg">1750.55</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.72658107</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </OperationalEquipment> + </OperatorsItems> + <NotAllocated Desc="Nicht zugeordnete Massenanteile und Schwerpunktlage des Massenelements"> + <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass> + <RefPoint Desc="position of mass item to global point of reference"> + <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item> + <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item> + <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item> + </RefPoint> + </NotAllocated> + </MassBreakdown> + <MTM Desc="Maximum Taxi Mass" ToolLevel="1" Unit="kg">0</MTM> + <MLM Desc="Maximum Landing Mass" ToolLevel="1" Unit="kg">65025.01668</MLM> + <MTOM Desc="Maximum Take-Off Mass" ToolLevel="3" Unit="kg">80000</MTOM> + <MRM Desc="Maximum Ramp Mass" ToolLevel="1" Unit="kg">0</MRM> + <MME Desc="Manufacturing Mass Empty" ToolLevel="1" Unit="kg">38656.38017</MME> + <OME Desc="Operating Mass Empty" ToolLevel="1" Unit="kg">999</OME> + <MZFM Desc="Maximum Zero Fuel Mass" ToolLevel="1" Unit="kg">61982.79523</MZFM> + <MaximumPayload Desc="Maximale Nutzlast" ToolLevel="1" Unit="kg">20000</MaximumPayload> + <MaximumUsableFuel Desc="Benutzbare Kraftstoffmasse" ToolLevel="1" Unit="kg">31084.34394</MaximumUsableFuel> + <WingLoading Desc="Fluegelflaechenlast" ToolLevel="1" Unit="kg/m2">628.681385</WingLoading> + <ThrustToWeight Desc="Schubkraft (kN) zu Gewichtskrafthaeltnis (kN)" ToolLevel="1" Unit="-">0.3218120393</ThrustToWeight> + <PowerToWeight Desc="Leistungsgewicht" ToolLevel="1" Unit="kW/kg">0</PowerToWeight> + <MomentsOfInertia Desc="Flaechentraegheitsmomente"> + <Ixx Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixx> + <Iyy Desc="-" ToolLevel="1" Unit="kg*m2">0</Iyy> + <Izz Desc="-" ToolLevel="1" Unit="kg*m2">0</Izz> + <Ixy Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixy> + <Ixz Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixz> + <Iyz Desc="-" ToolLevel="1" Unit="kg*m2">0</Iyz> + </MomentsOfInertia> + <CentreOfGravityRange Desc="Schwerpunktsgrenzen"> + <TrimRefPt Desc="Schwerpunktlage fuer CM-Berechnung und Trimmung im Reiseflug"> + <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.7359472859</h> + <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.56950713</r> + <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y> + </TrimRefPt> + <ForwardLimit Desc="Vorderste Schwerpunktlage"> + <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.9505895064</h> + <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.4584795</r> + <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y> + </ForwardLimit> + <AftLimit Desc="Hinterste Schwerpunktlage"> + <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-1.011726725</h> + <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.65854294</r> + <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y> + </AftLimit> + </CentreOfGravityRange> + </MassesAndLoadings> + <Geometry Desc="Geometriebeschreibung"> + <UsedElements Desc="Liste der verwendeten Geometrieelemente"> + <LiftingSurfaces Desc="Anzahl der verwendeten Elemente LiftingSurface" ToolLevel="1">2</LiftingSurfaces> + <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="1" ToolLevel="1" Unit="-">MainWing</LiftingSurface> + <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="2" ToolLevel="1" Unit="-">Stabiliser</LiftingSurface> + <VerticalSurfaces Desc="Anzahl der verwendeten Elemente VerticalSurface" ToolLevel="1">1</VerticalSurfaces> + <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="1" ToolLevel="1" Unit="-">Fin</VerticalSurface> + <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="2" ToolLevel="1" Unit="-">0</VerticalSurface> + <Fuselages Desc="Anzahl der verwendeten Elemente Fuselage" ToolLevel="1">1</Fuselages> + <Fuselage Desc="Name des verwendeten Fuselage-Elements" ID="1" ToolLevel="1" Unit="-">Fuselage</Fuselage> + <Nacelles Desc="Anzahl der verwendeten Elemente Nacelle" ToolLevel="1">2</Nacelles> + <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingNacelle</Nacelle> + <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingNacelle</Nacelle> + <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="3" ToolLevel="1" Unit="-">0</Nacelle> + <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="4" ToolLevel="1" Unit="-">0</Nacelle> + <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="5" ToolLevel="1" Unit="-">0</Nacelle> + <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="6" ToolLevel="1" Unit="-">0</Nacelle> + <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="7" ToolLevel="1" Unit="-">0</Nacelle> + <Pylons Desc="Anzahl der verwendeten Elemente Pylon" ToolLevel="1">2</Pylons> + <Pylon Desc="Name des verwendeten Pylon-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingPylon</Pylon> + <Pylon Desc="Name des verwendeten Pylon-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingPylon</Pylon> + <Pylon Desc="Name des verwendeten Pylon-Elements" ID="3" ToolLevel="1" Unit="-">0</Pylon> + <Pylon Desc="Name des verwendeten Pylon-Elements" ID="4" ToolLevel="1" Unit="-">0</Pylon> + <Pylon Desc="Name des verwendeten Pylon-Elements" ID="5" ToolLevel="1" Unit="-">0</Pylon> + <Pylon Desc="Name des verwendeten Pylon-Elements" ID="6" ToolLevel="1" Unit="-">0</Pylon> + <Gears Desc="Anzahl der verwendeten Elemente Gear" ToolLevel="1">3</Gears> + <Gear Desc="Name des verwendeten Gear-Elements" ID="1" ToolLevel="1" Unit="-">NoseGear</Gear> + <Gear Desc="Name des verwendeten Gear-Elements" ID="2" ToolLevel="1" Unit="-">OuterRightMainGear</Gear> + <Gear Desc="Name des verwendeten Gear-Elements" ID="3" ToolLevel="1" Unit="-">OuterLeftMainGear</Gear> + <Gear Desc="Name des verwendeten Gear-Elements" ID="4" ToolLevel="1" Unit="-">0</Gear> + <Gear Desc="Name des verwendeten Gear-Elements" ID="5" ToolLevel="1" Unit="-">0</Gear> + </UsedElements> + <LiftingSurface Desc="Beschreibung des Hauptfluegels" ID="MainWing"> + <SurfaceRefPoint Desc="position of wing to global point of reference"> + <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Surface> + <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface> + <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Surface> + </SurfaceRefPoint> + <SurfaceParameters Desc="Parametric description of lifting surface geometry"> + <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric> + <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation> + <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">0</i_Surface> + <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">200</SectionPoints> + <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1"> + <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">2</HalfSurfaceSegments> + <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_15.dat</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_12.dat</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">6.969546741</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.363049953</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">5.115537999</s_Segment> + <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.091406079</nu_Segment> + <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.11</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.55</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.16</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.65</l_rel_o_RearSpar> + </HalfSurfaceSegment> + <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="Surface"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_12.dat</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_11.dat</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.363049953</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.036840684</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">11.93625533</s_Segment> + <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.374274265</nu_Segment> + <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.16</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.27</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar> + </HalfSurfaceSegment> + <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar> + </HalfSurfaceSegment> + <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen"> + <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">8</TEDevices> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1184861071</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.2</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.78</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Aileron</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.8</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.98</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerGround</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2062430536</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.125</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.25</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.4195</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.4195</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.533</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.533</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.6465</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.6465</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.76</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">1</LEDevices> + <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1"> + <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">Slat</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1184861071</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.11</l_rel_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.27</l_rel_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">35</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </LEDevice> + </ControlDeviceSetup> + </HalfSurfaceDescription> + <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2"> + <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments> + <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar> + </HalfSurfaceSegment> + <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen"> + <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices> + <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1"> + <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </LEDevice> + </ControlDeviceSetup> + </HalfSurfaceDescription> + </SurfaceParameters> + </LiftingSurface> + <LiftingSurface Desc="Beschreibung des Hoehenleitwerks" ID="Stabiliser"> + <SurfaceRefPoint Desc="position of wing to global point of reference"> + <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">31.1606612</r_Surface> + <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface> + <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Surface> + </SurfaceRefPoint> + <SurfaceParameters Desc="Parametric description of lifting surface geometry"> + <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric> + <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation> + <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">-1.140234056</i_Surface> + <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints> + <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1"> + <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">1</HalfSurfaceSegments> + <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.962556849</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.11563951</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.392179667</s_Segment> + <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">31.99999988</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.15</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.3</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar> + </HalfSurfaceSegment> + <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar> + </HalfSurfaceSegment> + <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen"> + <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1"> + <Type Desc="Typ der Hinterkantenflaeche (Elevator)" ToolLevel="1">Elevator</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg> + </DeflectionAngle> + </TEDevice> + <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices> + <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1"> + <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </LEDevice> + </ControlDeviceSetup> + </HalfSurfaceDescription> + <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2"> + <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments> + <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar> + </HalfSurfaceSegment> + <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen"> + <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8"> + <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </TEDevice> + <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices> + <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1"> + <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg> + </DeflectionAngle> + </LEDevice> + </ControlDeviceSetup> + </HalfSurfaceDescription> + </SurfaceParameters> + </LiftingSurface> + <VerticalSurface Desc="Beschreibung des Seitenleitwerks" ID="Fin"> + <SurfaceRefPoint Desc="Referenzpunkt der vertikalen Steuerflaeche"> + <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">29.20843962</r_Surface> + <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface> + <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">1.692105859</h_Surface> + </SurfaceRefPoint> + <SurfaceParameters Desc="Parametric description of vertical surface geometry"> + <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints> + <SurfaceSegments Desc="Number of segments in this vertical surface" ToolLevel="1">1</SurfaceSegments> + <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">5.914778427</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.564960467</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">7.105751949</s_Segment> + <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">38.99999987</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment> + <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment> + <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar> + <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar> + <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar> + <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar> + </SurfaceSegment> + <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen"> + <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices> + <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1"> + <Type Desc="Typ der Hinterkantenflaeche (Rudder)" ToolLevel="1">Rudder</Type> + <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i> + <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i> + <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o> + <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o> + <DeflectionAngle Desc="Steuerflaechenausschlagwinkel"> + <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos> + <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg> + </DeflectionAngle> + </TEDevice> + </ControlDeviceSetup> + </SurfaceParameters> + </VerticalSurface> + <Fuselage Desc="Beschreibung des Rumpfes" ID="Fuselage"> + <FuselageRefPoint Desc="position of the fuselage nose refpoint to global point of reference"> + <r_Fuselage Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Fuselage> + <y_Fuselage Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Fuselage> + <h_Fuselage Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Fuselage> + </FuselageRefPoint> + <FuselageParameters Desc="parametric description of the fuselage"> + <NoseDescription> + <NoseSegments Desc="No of nose segments" ToolLevel="1">9</NoseSegments> + <TipSegment> + <h_Tip Desc="offset of nosetip" ToolLevel="1" Unit="m">-0.5351396212</h_Tip> + </TipSegment> + <NoseSegment ID="1"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.6205763694</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.6626671728</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.06782437376</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.5351396212</deltah_Segment> + </NoseSegment> + <NoseSegment ID="2"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.229534829</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.312928447</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.2034731213</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.4376004301</deltah_Segment> + </NoseSegment> + <NoseSegment ID="3"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.814885649</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.937980885</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.3391218688</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.3438425644</deltah_Segment> + </NoseSegment> + <NoseSegment ID="4"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.363843474</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.524171961</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.4747706164</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.2559139029</deltah_Segment> + </NoseSegment> + <NoseSegment ID="5"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.862283086</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.05641841</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.6104193639</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1760769356</deltah_Segment> + </NoseSegment> + <NoseSegment ID="6"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.293963779</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.517377993</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.7460681114</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1069329983</deltah_Segment> + </NoseSegment> + <NoseSegment ID="7"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.639314251</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.886151978</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.8817168589</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.05161690045</deltah_Segment> + </NoseSegment> + <NoseSegment ID="8"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.873337327</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136047749</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.017365606</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.01413253478</deltah_Segment> + </NoseSegment> + <NoseSegment ID="9"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.230264648</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.153014354</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0</deltah_Segment> + </NoseSegment> + </NoseDescription> + <MidSectionDescription> + <MidSectionSegments Desc="No of mid-segment segments" ToolLevel="1">1</MidSectionSegments> + <MidSectionSegment ID="1"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.230264648</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">15.57908662</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment> + </MidSectionSegment> + <MidSectionSegment ID="2"> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment> + </MidSectionSegment> + </MidSectionDescription> + <TailDescription> + <TailSegments Desc="No of tail segments" ToolLevel="1">7</TailSegments> + <TailSegment ID="1"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.163206861</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.0335288931</deltah_Segment> + </TailSegment> + <TailSegment ID="2"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.960934992</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.1346648278</deltah_Segment> + </TailSegment> + <TailSegment ID="3"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.893957495</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.620061515</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.3051015662</deltah_Segment> + </TailSegment> + <TailSegment ID="4"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.614493823</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.151622366</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.539321141</deltah_Segment> + </TailSegment> + <TailSegment ID="5"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.115516897</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.662987184</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.7836387319</deltah_Segment> + </TailSegment> + <TailSegment ID="6"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.980784913</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.754520057</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.390445476</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.237872295</deltah_Segment> + </TailSegment> + <TailSegment ID="7"> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.8460529295</w_Segment> + <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.8460529295</h_Segment> + <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.390445476</l_Segment> + <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.692105859</deltah_Segment> + </TailSegment> + </TailDescription> + </FuselageParameters> + </Fuselage> + <Nacelle Desc="Beschreibung der inneren rechten Triebwerksgondel" ID="InnerRightWingNacelle"> + <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs"> + <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.1833365</r_Nacelle> + <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">5.219203967</y_Nacelle> + <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Nacelle> + </NacelleRefPoint> + <NacelleParameters Desc="parametric description of the nacelle"> + <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle> + <Points Desc="No of points describing the section" ToolLevel="1">20</Points> + <Segments Desc="No of segments" ToolLevel="1">2</Segments> + <InletSegment> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_Inlet> + <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_Inlet> + <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.627</l_Inlet> + </InletSegment> + <NacelleSegment ID="1"> + <InnerSegmentPointData ToolLevel="1">fuselage.dat</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">fuselage.dat</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.28625</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.6475</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.254</l_Segment> + </NacelleSegment> + <NacelleSegment ID="2"> + <InnerSegmentPointData ToolLevel="1">fuselage.dat</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">fuselage.dat</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.28625</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.6475</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.627</l_Segment> + </NacelleSegment> + <NacelleSegment ID="3"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <NacelleSegment ID="4"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <ExitSegment> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_Exit> + <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_Exit> + </ExitSegment> + </NacelleParameters> + <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID> + </Nacelle> + <Nacelle Desc="Beschreibung der inneren linken Triebwerksgondel" ID="InnerLeftWingNacelle"> + <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs"> + <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.1833365</r_Nacelle> + <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-5.219203967</y_Nacelle> + <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Nacelle> + </NacelleRefPoint> + <NacelleParameters Desc="parametric description of the nacelle"> + <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle> + <Points Desc="No of points describing the section" ToolLevel="1">20</Points> + <Segments Desc="No of segments" ToolLevel="1">2</Segments> + <InletSegment> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_Inlet> + <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_Inlet> + <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.627</l_Inlet> + </InletSegment> + <NacelleSegment ID="1"> + <InnerSegmentPointData ToolLevel="1">fuselage.dat</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">fuselage.dat</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.28625</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.6475</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.254</l_Segment> + </NacelleSegment> + <NacelleSegment ID="2"> + <InnerSegmentPointData ToolLevel="1">fuselage.dat</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">fuselage.dat</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.28625</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.6475</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.627</l_Segment> + </NacelleSegment> + <NacelleSegment ID="3"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <NacelleSegment ID="4"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <ExitSegment> + <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData> + <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_Exit> + <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_Exit> + </ExitSegment> + </NacelleParameters> + <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID> + </Nacelle> + <Nacelle Desc="Beschreibung der aeusseren rechten Triebwerksgondel" ID="OuterRightWingNacelle"> + <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs"> + <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle> + <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle> + <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle> + </NacelleRefPoint> + <NacelleParameters Desc="parametric description of the nacelle"> + <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle> + <Points Desc="No of points describing the section" ToolLevel="1">0</Points> + <Segments Desc="No of segments" ToolLevel="1">0</Segments> + <InletSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet> + <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet> + <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet> + </InletSegment> + <NacelleSegment ID="1"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <NacelleSegment ID="2"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <ExitSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit> + <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit> + </ExitSegment> + </NacelleParameters> + <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID> + </Nacelle> + <Nacelle Desc="Beschreibung der aeusseren linken Triebwerksgondel" ID="OuterLeftWingNacelle"> + <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs"> + <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle> + <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle> + <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle> + </NacelleRefPoint> + <NacelleParameters Desc="parametric description of the nacelle"> + <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle> + <Points Desc="No of points describing the section" ToolLevel="1">0</Points> + <Segments Desc="No of segments" ToolLevel="1">0</Segments> + <InletSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet> + <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet> + <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet> + </InletSegment> + <NacelleSegment ID="1"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <NacelleSegment ID="2"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <ExitSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit> + <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit> + </ExitSegment> + </NacelleParameters> + <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID> + </Nacelle> + <Nacelle Desc="Beschreibung der rechten Hecktriebwerksgondel" ID="RightFuselageNacelle"> + <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs"> + <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle> + <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle> + <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle> + </NacelleRefPoint> + <NacelleParameters Desc="parametric description of the nacelle"> + <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle> + <Points Desc="No of points describing the section" ToolLevel="1">0</Points> + <Segments Desc="No of segments" ToolLevel="1">0</Segments> + <InletSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet> + <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet> + <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet> + </InletSegment> + <NacelleSegment ID="1"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <NacelleSegment ID="2"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <ExitSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit> + <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit> + </ExitSegment> + </NacelleParameters> + <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID> + </Nacelle> + <Nacelle Desc="Beschreibung der linken Hecktriebwerksgondel" ID="LeftFuselageNacelle"> + <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs"> + <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle> + <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle> + <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle> + </NacelleRefPoint> + <NacelleParameters Desc="parametric description of the nacelle"> + <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle> + <Points Desc="No of points describing the section" ToolLevel="1">0</Points> + <Segments Desc="No of segments" ToolLevel="1">0</Segments> + <InletSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet> + <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet> + <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet> + </InletSegment> + <NacelleSegment ID="1"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <NacelleSegment ID="2"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <ExitSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit> + <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit> + </ExitSegment> + </NacelleParameters> + <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID> + </Nacelle> + <Nacelle Desc="Beschreibung der in das SLW integrierten Triebwerksgondel" ID="FinNacelle"> + <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs"> + <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle> + <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle> + <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle> + </NacelleRefPoint> + <NacelleParameters Desc="parametric description of the nacelle"> + <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle> + <Points Desc="No of points describing the section" ToolLevel="1">0</Points> + <Segments Desc="No of segments" ToolLevel="1">0</Segments> + <InletSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet> + <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet> + <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet> + </InletSegment> + <NacelleSegment ID="1"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <NacelleSegment ID="2"> + <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData> + <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData> + <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment> + <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment> + <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment> + <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment> + <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment> + </NacelleSegment> + <ExitSegment> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit> + <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit> + </ExitSegment> + </NacelleParameters> + <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID> + </Nacelle> + <Pylon Desc="Beschreibung des Pylons" ID="InnerRightWingPylon"> + <SurfaceRefPoint Desc="Referenzpunkt des Pylons"> + <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.4341365</r_Surface> + <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">5.219203967</y_Surface> + <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Surface> + </SurfaceRefPoint> + <SurfaceParameters Desc="Parametric description of pylon geometry"> + <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints> + <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments> + <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.0096</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">3.762</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.11195</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.762</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.11583452</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.7413</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.91922836</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + </SurfaceParameters> + </Pylon> + <Pylon Desc="Beschreibung des Pylons" ID="InnerLeftWingPylon"> + <SurfaceRefPoint Desc="Referenzpunkt des Pylons"> + <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.4341365</r_Surface> + <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">-5.219203967</y_Surface> + <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Surface> + </SurfaceRefPoint> + <SurfaceParameters Desc="Parametric description of pylon geometry"> + <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints> + <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments> + <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.0096</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">3.762</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.11195</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.762</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.11583452</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.7413</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.91922836</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + </SurfaceParameters> + </Pylon> + <Pylon Desc="Beschreibung des Pylons" ID="OuterRightWingPylon"> + <SurfaceRefPoint Desc="Referenzpunkt des Pylons"> + <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface> + <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface> + <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface> + </SurfaceRefPoint> + <SurfaceParameters Desc="Parametric description of pylon geometry"> + <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints> + <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments> + <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + </SurfaceParameters> + </Pylon> + <Pylon Desc="Beschreibung des Pylons" ID="OuterLeftWingPylon"> + <SurfaceRefPoint Desc="Referenzpunkt des Pylons"> + <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface> + <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface> + <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface> + </SurfaceRefPoint> + <SurfaceParameters Desc="Parametric description of pylon geometry"> + <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints> + <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments> + <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + </SurfaceParameters> + </Pylon> + <Pylon Desc="Beschreibung des Pylons" ID="RightFuselagePylon"> + <SurfaceRefPoint Desc="Referenzpunkt des Pylons"> + <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface> + <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface> + <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface> + </SurfaceRefPoint> + <SurfaceParameters Desc="Parametric description of pylon geometry"> + <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints> + <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments> + <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + </SurfaceParameters> + </Pylon> + <Pylon Desc="Beschreibung des Pylons" ID="LeftFuselagePylon"> + <SurfaceRefPoint Desc="Referenzpunkt des Pylons"> + <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface> + <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface> + <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface> + </SurfaceRefPoint> + <SurfaceParameters Desc="Parametric description of pylon geometry"> + <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints> + <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments> + <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0"> + <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment> + <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment> + <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment> + <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment> + <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment> + <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment> + <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment> + <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment> + </SurfaceSegment> + </SurfaceParameters> + </Pylon> + <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear"> + <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks"> + <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.662516183</r_Gear> + <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear> + <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.023847396</h_Gear> + </GearRefPoint> + <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen."> + <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.662516183</r_Wheelgroup> + <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup> + <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.834540304</h_Wheelgroup> + </WheelGroupRefPoint> + <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.127127</StrutDiameter> + <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable> + <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)"> + <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x> + <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y> + <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z> + </HingeAxis> + <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle> + <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase> + <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.3911791258</Wheeltrack> + <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes> + <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis> + <Wheel Desc="Beschreibung des Rades"> + <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0.6858</TireDiameter> + <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.19558</TireWidth> + <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.3429</RimDiameter> + </Wheel> + </Gear> + <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear"> + <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks"> + <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.63676778</r_Gear> + <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.076078967</y_Gear> + <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.371848143</h_Gear> + </GearRefPoint> + <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen."> + <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.5474552</r_Wheelgroup> + <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.076078967</y_Wheelgroup> + <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.593240304</h_Wheelgroup> + </WheelGroupRefPoint> + <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter> + <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable> + <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)"> + <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x> + <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y> + <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z> + </HingeAxis> + <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">-90</RetractionAngle> + <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase> + <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack> + <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes> + <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis> + <Wheel Desc="Beschreibung des Rades"> + <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter> + <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth> + <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter> + </Wheel> + </Gear> + <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear"> + <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks"> + <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.63676778</r_Gear> + <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.076078967</y_Gear> + <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.371848143</h_Gear> + </GearRefPoint> + <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen."> + <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.5474552</r_Wheelgroup> + <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.076078967</y_Wheelgroup> + <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.593240304</h_Wheelgroup> + </WheelGroupRefPoint> + <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter> + <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable> + <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)"> + <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x> + <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y> + <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z> + </HingeAxis> + <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle> + <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase> + <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack> + <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes> + <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis> + <Wheel Desc="Beschreibung des Rades"> + <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter> + <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth> + <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter> + </Wheel> + </Gear> + <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear"> + <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks"> + <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear> + <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear> + <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear> + </GearRefPoint> + <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen."> + <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup> + <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup> + <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup> + </WheelGroupRefPoint> + <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter> + <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable> + <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)"> + <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x> + <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y> + <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z> + </HingeAxis> + <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle> + <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase> + <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack> + <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes> + <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis> + <Wheel Desc="Beschreibung des Rades"> + <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter> + <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth> + <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter> + </Wheel> + </Gear> + <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear"> + <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks"> + <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear> + <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear> + <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear> + </GearRefPoint> + <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen."> + <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup> + <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup> + <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup> + </WheelGroupRefPoint> + <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter> + <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable> + <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)"> + <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x> + <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y> + <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z> + </HingeAxis> + <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle> + <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase> + <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack> + <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes> + <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis> + <Wheel Desc="Beschreibung des Rades"> + <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter> + <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth> + <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter> + </Wheel> + </Gear> + </Geometry> + <Structure Desc="Strukturdaten"></Structure> + <Accommodation Desc="Kabineneinrichtung"> + <PassengersTotal Desc="Gesamtanzahl der Sitzplaetze" ToolLevel="1">150</PassengersTotal> + <FlightCrew Desc="Anzahl Cockpitbesatzung" ToolLevel="1">2</FlightCrew> + <CabinCrew Desc="Anzahl Flugbegleiter" ToolLevel="1">4</CabinCrew> + <Seats Desc="Description of seats"> + <NoOfSeatTypes Desc="Anzahl der Sitzklassen" ToolLevel="1">5</NoOfSeatTypes> + <seat Desc="Description of seat" ID="1"> + <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">commuter</seatClassType> + <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">1</noOfSeatConfigurations> + <seatConfiguration Desc="Description of SeatConfiguration" ID="1"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">15</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="2"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="3"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="4"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="5"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats> + </seatConfiguration> + <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE> + <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0</massIFE> + </seat> + <seat Desc="Description of seat" ID="2"> + <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">economy</seatClassType> + <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">4</noOfSeatConfigurations> + <seatConfiguration Desc="Description of SeatConfiguration" ID="1"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">9</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="2"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">14</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="3"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">19.5</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="4"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">4</noOfSeats> + </seatConfiguration> + <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE> + <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE> + </seat> + <seat Desc="Description of seat" ID="3"> + <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">GeneralAviation</seatClassType> + <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">2</noOfSeatConfigurations> + <seatConfiguration Desc="Description of SeatConfiguration" ID="1"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">15</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="2"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25.1</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats> + </seatConfiguration> + <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE> + <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0</massIFE> + </seat> + <seat Desc="Description of seat" ID="4"> + <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">business</seatClassType> + <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">3</noOfSeatConfigurations> + <seatConfiguration Desc="Description of SeatConfiguration" ID="1"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">27.2</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="2"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">35.1</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="3"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats> + </seatConfiguration> + <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE> + <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE> + </seat> + <seat Desc="Description of seat" ID="5"> + <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">first</seatClassType> + <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">2</noOfSeatConfigurations> + <seatConfiguration Desc="Description of SeatConfiguration" ID="1"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">21.25</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="2"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">42.5</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats> + </seatConfiguration> + <seatConfiguration Desc="Description of SeatConfiguration" ID="3"> + <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass> + <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats> + </seatConfiguration> + <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE> + <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE> + </seat> + </Seats> + <Galleys Desc="Description of galleys"> + <NoOfGalleyTypes Desc="Anzahl verwendeter Kuechen Typen" ToolLevel="1">2</NoOfGalleyTypes> + <Gal Desc="Description of galley" ID="1"> + <nameGalley Desc="Name of galley" ToolLevel="1">large_galley</nameGalley> + <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys> + <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">226.8</mass> + <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">14418</power> + </Gal> + <Gal Desc="Description of galley" ID="2"> + <nameGalley Desc="Name of galley" ToolLevel="1">small_galley</nameGalley> + <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys> + <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">61.24</mass> + <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">3887</power> + </Gal> + <Gal Desc="Description of galley" ID="3"> + <nameGalley Desc="Name of galley" ToolLevel="1">0</nameGalley> + <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">0</NumberOfGalleys> + <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">0</mass> + <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">0</power> + </Gal> + </Galleys> + <Lavatories Desc="Description of lavatories"> + <NoOfLavatoryTypes Desc="Anzahl verwendeter Lavatorie-Typen" ToolLevel="1">1</NoOfLavatoryTypes> + <Lav Desc="Description of lavatory" ID="1"> + <nameLavatory Desc="Name of lavatory" ToolLevel="1">standard_lavatory</nameLavatory> + <NumberOfLavatories Desc="Gesamtzahl der verwendeten Lavatories dieses Typs" ToolLevel="1">3</NumberOfLavatories> + <mass Desc="Masse einer Lavatoryeinheit" ToolLevel="1" Unit="kg">96.67</mass> + </Lav> + </Lavatories> + <Cabin Desc="Beschreibung der Kabine"> + <V_AirConditioned Desc="Klimatisiertes Kabinenvolumen gesamt" ToolLevel="1" Unit="m3">190.47918</V_AirConditioned> + <CabinDecks Desc="Anzahl Kabinendecks" ToolLevel="1">1</CabinDecks> + <CabinDeck Desc="Parameter eines Kabinendecks" ID="1"> + <A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">95.53300238</A_CabinDeck> + <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">2.13</h_CabinDeck> + <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">3.613074406</w_CabinDeck> + <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">26.44091752</l_CabinDeck> + <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">185.9285625</V_CabinDeck> + <PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">150</PAX_CabinDeck> + <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">2</Classes> + <Class Desc="Definition der Klasse" ID="1"> + <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">6.044387137</x_center> + </Class> + <Class Desc="Definition der Klasse" ID="2"> + <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">19.2648459</x_center> + </Class> + <Class Desc="Definition der Klasse" ID="3"> + <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center> + </Class> + </CabinDeck> + <CabinDeck Desc="Parameter eines Kabinendecks" ID="2"> + <A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">0</A_CabinDeck> + <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">0</h_CabinDeck> + <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">0</w_CabinDeck> + <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">0</l_CabinDeck> + <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">0</V_CabinDeck> + <PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">0</PAX_CabinDeck> + <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">0</Classes> + <Class Desc="Definition der Klasse" ID="1"> + <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center> + </Class> + <Class Desc="Definition der Klasse" ID="2"> + <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center> + </Class> + <Class Desc="Definition der Klasse" ID="3"> + <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center> + </Class> + </CabinDeck> + </Cabin> + <Cargo Desc="Beschreibung des Frachtraums"> + <V_Cargo Desc="Frachtvolumen gesamt" ToolLevel="1" Unit="m3">33.22757663</V_Cargo> + <CargoDecks Desc="Anzahl Frachtdecks" ToolLevel="1">1</CargoDecks> + <CargoDeck Desc="Parameter eines Frachtdecks" ID="1"> + <A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">55.02284727</A_CargoDeck> + <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">1.14</h_CargoDeck> + <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">3.252922327</w_CargoDeck> + <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">16.91489736</l_CargoDeck> + <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">34.30498624</V_CargoDeck> + <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">12.17849076</V_BulkCargo> + <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">2</Compartments> + <Compartment Desc="Definition des Compartments" ID="1"> + <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">4.69</Length> + <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">6.045</x_center> + </Compartment> + <Compartment Desc="Definition des Compartments" ID="2"> + <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">6.22</Length> + <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">23.42652858</x_center> + </Compartment> + <Compartment Desc="Definition des Compartments" ID="3"> + <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length> + <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center> + </Compartment> + </CargoDeck> + <CargoDeck Desc="Parameter eines Frachtdecks" ID="2"> + <A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">0</A_CargoDeck> + <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">0</h_CargoDeck> + <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">0</w_CargoDeck> + <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">0</l_CargoDeck> + <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">0</V_CargoDeck> + <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">0</V_BulkCargo> + <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">0</Compartments> + <Compartment Desc="Definition des Compartments" ID="1"> + <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length> + <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center> + </Compartment> + <Compartment Desc="Definition des Compartments" ID="2"> + <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length> + <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center> + </Compartment> + <Compartment Desc="Definition des Compartments" ID="3"> + <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length> + <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center> + </Compartment> + </CargoDeck> + </Cargo> + </Accommodation> + <Propulsion Desc="Angabe der verwendeten Engine Types (nicht jede einzelne Engine)"> + <NumberOfEngineTypes Desc="Anzahl verschiedener Triebwerkstypen" ToolLevel="1">0</NumberOfEngineTypes> + <Engine Desc="Triebwerks-/Motortyp" ID="1"> + <TypeOfEngine Desc="Triebwerkstyp z.Zt. Jet oder Prop" ToolLevel="1" Unit="-">jet</TypeOfEngine> + <EngineModel Desc="Triebwerksmodell fuer Gummimotor" ToolLevel="1" Unit="-">V2527-A5</EngineModel> + <NumberOfEngines Desc="Anzahl der Triebwerke - notwendig?" ToolLevel="1">2</NumberOfEngines> + <ScaleEngines Desc="Skalierungsfaktor fuer das Triebwerksmodell i.S.e. Gummimotors" ToolLevel="1" Unit="-">1.039876757</ScaleEngines> + <ScaleFuelFlow Desc="Skalierungsfaktor fuer den Fuel Flow" ToolLevel="1" Unit="-">1</ScaleFuelFlow> + <EngineDataFile Desc="Name der Triebewerksdatei (enthaelt Geometriedaten und Decks)" ToolLevel="1" Unit="-">V2527-A5/V2527-A5.xml</EngineDataFile> + <JetEngineData Desc="Jet spezifische Triebwerksdaten"> + <SeaLevelStaticThrust Desc="Flat-Rated Standschub" ToolLevel="1" Unit="kN">121.4507148</SeaLevelStaticThrust> + <FanDiameter Desc="Durchmesser des Fans" ToolLevel="1" Unit="m">1.613</FanDiameter> + </JetEngineData> + <TurbopropEngineData Desc="Prop spezifische Triebwerksdaten"> + <Prop Desc="Propellerdaten"> + <PropDiameter Desc="Propellerdurchmesser" ToolLevel="1" Unit="m">0</PropDiameter> + <PropBlades Desc="Anzahl Propellerblaetter" ToolLevel="1">0</PropBlades> + <SegmentPointData ToolLevel="1">0</SegmentPointData> + <Pitch Desc="Variable oder Fix Pitch" ToolLevel="1">0</Pitch> + <Thickness Desc="Thickness of rotor disc " ToolLevel="1" Unit="m">0</Thickness> + </Prop> + <P_shp Desc="Triebwerkswellenleistung" ToolLevel="1" Unit="kW">0</P_shp> + </TurbopropEngineData> + <EngineDimensions Desc="Geometrische Abmasse des skalierten Triebwerks, Kerntriebwerk"> + <w_Engine Desc="Breite des uninstallierten Triebwerks" ToolLevel="1" Unit="m">1.829</w_Engine> + <h_Engine Desc="Hoehe des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.118</h_Engine> + <l_Engine Desc="Gesamtlaenge des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.508</l_Engine> + </EngineDimensions> + <NacelleRescaling Desc="Parameter fuer Rescaling der Wing Nacelles" Matched="0"> + <InnerNacelle> + <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos> + <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos> + <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos> + <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio> + <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio> + <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio> + </InnerNacelle> + <OuterNacelle> + <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos> + <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos> + <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos> + <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio> + <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio> + <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio> + </OuterNacelle> + </NacelleRescaling> + <ScaledPerformanceCharacteristics Desc="Leistungscharakteristik des (eines!) skalierten Triebwerks"> + <EquivalentThrust Desc="1.25 * Max-Go-Around (Schub bei ISA+15, SL, Ma0.25, N1 100 perc)" ToolLevel="1" Unit="kN">121.6192213</EquivalentThrust> + <MaximumTakeOff Desc="Maximale Startschubbedingung bei ISA+15 und keinen Off-takes bei Altitude_ft=0.0 Mach=0.0"> + <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">121.4507148</Thrust> + <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.255306839</FuelFlow> + <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01033593619</TSFC> + <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1.027199488</N1> + </MaximumTakeOff> + <MaximumGoAround Desc="Maximale Go-Around-Bedingung bei ISA+15 und keinen Off-takes bei Altitude_ft=0.0, Mach=0.25"> + <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">97.29537705</Thrust> + <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.274976051</FuelFlow> + <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01310417914</TSFC> + <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1.02423458</N1> + </MaximumGoAround> + <MaximumContinous Altitude_ft="35000" Desc="Maximales Schublimit ohne Zeitlimit bei ISA+0 bei" Mach="0.78"> + <MaxThrust Desc="Without Offtakes"> + <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">35.65209987</Thrust> + <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.6237266005</FuelFlow> + <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01749480683</TSFC> + <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1</N1> + </MaxThrust> + <BucketThrust Desc="Without Offtakes"> + <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">25.92001194</Thrust> + <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4343473894</FuelFlow> + <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01675722181</TSFC> + <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.875</N1> + </BucketThrust> + <BucketThrustOfftakes Desc="With Average Cruise Offtakes (s. Design Mission)"> + <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">25.97268447</Thrust> + <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4521939534</FuelFlow> + <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01741036641</TSFC> + <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.905</N1> + </BucketThrustOfftakes> + </MaximumContinous> + </ScaledPerformanceCharacteristics> + <UsedForNacelles Desc="Angabe der Nacelle IDs, in welche dieser Engine Type eingebaut wird"> + <UsedForNumberOfEngines ToolLevel="1">0</UsedForNumberOfEngines> + <NacelleID ID="1" ToolLevel="1">0</NacelleID> + <NacelleID ID="2" ToolLevel="1">0</NacelleID> + <NacelleID ID="3" ToolLevel="1">0</NacelleID> + <NacelleID ID="4" ToolLevel="1">0</NacelleID> + </UsedForNacelles> + </Engine> + </Propulsion> + <Systems> + <FuelTank Desc="Tank system Parameters"> + <CentreTanks Desc="No of centre tanks" ToolLevel="1">1</CentreTanks> + <CentreTank Desc="Center-Tank Beschreibung" ID="1"> + <RefPoint Desc="position of tank reference point in relation to global point of reference"> + <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83307738</r_Tank> + <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Tank> + <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.330577781</h_Tank> + </RefPoint> + <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">10165.96362</TankVolume> + </CentreTank> + <WingTanks Desc="No of wing tanks" ToolLevel="1">2</WingTanks> + <WingTank Desc="Fluegeltank-Beschreibung" ID="1"> + <RefPoint Desc="position of tank reference point in relation to global point of reference"> + <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.57026607</r_Tank> + <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">6.308425637</y_Tank> + <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.094307567</h_Tank> + </RefPoint> + <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">14715.96338</TankVolume> + </WingTank> + <WingTank Desc="Fluegeltank-Beschreibung" ID="2"> + <RefPoint Desc="position of tank reference point in relation to global point of reference"> + <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.57026607</r_Tank> + <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">-6.308425637</y_Tank> + <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.094307567</h_Tank> + </RefPoint> + <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">14715.96338</TankVolume> + </WingTank> + <TrimTanks Desc="No of trim tanks" ToolLevel="1">0</TrimTanks> + <TrimTank Desc="Trimmtank-Beschreibung" ID="1"> + <RefPoint Desc="position of tank reference point in relation to global point of reference"> + <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Tank> + <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Tank> + <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">0</h_Tank> + </RefPoint> + <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">0</TankVolume> + </TrimTank> + <TotalFuelVolume Desc="Gesamtes Kraftstoffvolumen aller Tanks" ToolLevel="1" Unit="l">39597.89037</TotalFuelVolume> + </FuelTank> + <ATA21_EnvironmentalControlSystem> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">25.96155032</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.315916839</BleedAir> + </DesignPower> + <AirflowPerPax Desc="Konstanter Luftmassenstrom pro Passagier" ToolLevel="1" Unit="lbs/min">0.75</AirflowPerPax> + <Recirculation Desc="Prozentualer Anteil der Kabinenluft, die wieder verwendet wird (0.0 - 1.0)" ToolLevel="1" Unit="-">0.4</Recirculation> + </ATA21_EnvironmentalControlSystem> + <ATA22_AutoFlight> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA22_AutoFlight> + <ATA23_Communication> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA23_Communication> + <ATA24_ElectricSystem> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA24_ElectricSystem> + <ATA25_Furnishing> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">18.92</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA25_Furnishing> + <ATA26_FireProtection> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA26_FireProtection> + <ATA27_FlightControlSystem> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">95.17958985</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA27_FlightControlSystem> + <ATA28_FuelSystem> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">11.89508876</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA28_FuelSystem> + <ATA29_HydraulicSystem> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">7.171489811</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + <Pressure Desc="Nenn-Druck des Hydrauliksystems" ToolLevel="1" Unit="psi">3000</Pressure> + </ATA29_HydraulicSystem> + <ATA30_IceRainProtection> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">14.0269</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.128183366</BleedAir> + </DesignPower> + </ATA30_IceRainProtection> + <ATA31_Instrumentation> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA31_Instrumentation> + <ATA32_LandingGear> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">67.03267969</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA32_LandingGear> + <ATA33_Lights> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">7.96874401</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA33_Lights> + <ATA34_Navigation> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA34_Navigation> + <ATA35_Oxygen> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir> + </DesignPower> + </ATA35_Oxygen> + <ATA36_BleedAir> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0.1286368529</BleedAir> + </DesignPower> + </ATA36_BleedAir> + <ATA49_APU> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-0</BleedAir> + </DesignPower> + </ATA49_APU> + <ATA70_PropulsionSystem> + <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung"> + <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">-142.0813445</Electric> + <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">-174.2129642</Hydraulic> + <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-2.708144271</BleedAir> + </DesignPower> + </ATA70_PropulsionSystem> + </Systems> + <Aerodynamics Desc="Aerodynamik"> + <LoverD_Cruise Desc="Beste Gleitzahl L/D im Reiseflug fuer (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">17.07161371</LoverD_Cruise> + <LiftCoefficients Desc="Auftriebsbeiwerte"> + <C_L_design Desc="Design Auftriebsbeiwert" ToolLevel="1" Unit="-">0.5388392246</C_L_design> + <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert Landekonfiguration" ToolLevel="1" Unit="-">2.910828613</C_LmaxLanding> + <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert Startkonfiguration" ToolLevel="1" Unit="-">2.511580029</C_LmaxT-O> + <C_LoptimumCruise Desc="Auftriebsbeiwert bei bestem LoverD bei (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">0.534</C_LoptimumCruise> + <C_L_opt_wing Desc="Auftriebsbeiwert bei bestem LoverD (Anteil Fluegel)" ToolLevel="1" Unit="-">0.56482909</C_L_opt_wing> + <C_L_opt_stab Desc="Auftriebsbeiwert bei bestem LoverD (Anteil HLW)" ToolLevel="1" Unit="-">-0.03082906473</C_L_opt_stab> + <C_LgroundRoll Desc="lift coefficient on ground for ground roll calculation" ToolLevel="1" Unit="-">0.4</C_LgroundRoll> + </LiftCoefficients> + <DragCoefficients Desc="Widerstandsbeiwerte (bei bestem L/D im Cruise, s.o.)"> + <C_D_total Desc="Widerstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.03127999549</C_D_total> + <C_D_ind Desc="induzierter Widerstandsbeiwert" ToolLevel="1" Unit="-">0.01011147857</C_D_ind> + <C_D_visc Desc="Reibungswiderstandsbeiwerte" ToolLevel="1" Unit="-"> + <C_D_visc_total Desc="Reibungswiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.01998021606</C_D_visc_total> + <C_D_visc_wing Desc="Reibungswiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.006065898162</C_D_visc_wing> + <C_D_visc_stab Desc="Reibungswiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0.001539217794</C_D_visc_stab> + <C_D_visc_fin Desc="Reibungswiderstandsbeiwert SLW" ToolLevel="1" Unit="-">0.001759127689</C_D_visc_fin> + <C_D_visc_fus Desc="Reibungswiderstandsbeiwert Rumpf" ToolLevel="1" Unit="-">0.006881721154</C_D_visc_fus> + <C_D_visc_nac Desc="Reibungswiderstandsbeiwert Nacelle" ToolLevel="1" Unit="-">0.001626766969</C_D_visc_nac> + <C_D_visc_misc Desc="Reibungswiderstandsbeiwert weitere" ToolLevel="1" Unit="-">0.002107484288</C_D_visc_misc> + </C_D_visc> + <C_D_wave Desc="Wellenwiderstandsbeiwerte" ToolLevel="1" Unit="-"> + <C_D_wave_total Desc="Wellenwiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.00118830087</C_D_wave_total> + <C_D_wave_wing Desc="Wellenwiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.00118830087</C_D_wave_wing> + <C_D_wave_stab Desc="Wellenwiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0</C_D_wave_stab> + </C_D_wave> + <EoW_DragFactor Desc="Drag factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_DragFactor> + </DragCoefficients> + <MomentCoefficients Desc="Momentenbeiwerte (getrimmt, bei bestem L/D im Cruise, s.o.)"> + <C_M_total Desc="Momentenbeiwert bei optimum Cruise" ToolLevel="1" Unit="-">-0.001284519415</C_M_total> + </MomentCoefficients> + <Polar Desc="Flugzeugpolare"> + <PolarFile Desc="Dateiname der Flugzeugpolare" ToolLevel="1" Unit="-">CSR_polar.xml</PolarFile> + <Configurations Desc="Anzahl der aerodynamischen Konfigurationen in der Polarendatei" ToolLevel="1">7</Configurations> + <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="1" ToolLevel="1" Type="Cruise">Clean</Configuration> + <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="2" ToolLevel="1" Type="Departure">TakeOff</Configuration> + <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="3" ToolLevel="1" Type="Departure">TakeOffLGRetracted</Configuration> + <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="4" ToolLevel="1" Type="Departure">Climb</Configuration> + <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="5" ToolLevel="1" Type="Approach">Approach</Configuration> + <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="6" ToolLevel="1" Type="Approach">ApproachLG</Configuration> + <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="7" ToolLevel="1" Type="Approach">Landing</Configuration> + </Polar> + <ReferenceValues Desc="Aerodynamische Bezugsgroessen"> + <b Desc="Total wing span" ToolLevel="1" Unit="m">34.10358666</b> + <MAC Desc="Mean aerodynamic chord" ToolLevel="1" Unit="m">4.331683874</MAC> + <S_ref Desc="Wing reference area" ToolLevel="1" Unit="m2">122.4268024</S_ref> + </ReferenceValues> + <MaxSpoilerFactor Desc="Faktor zur max. Widerstandserhoehung durch Spoiler" ToolLevel="1" Unit="-">2.5</MaxSpoilerFactor> + </Aerodynamics> + <StabilityAndControlCharacteristics Desc="Flugmechanik, Stabilitaet und Steuerbarkeit"> + <Stabiliser> + <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">1.03545133</VolumeCoefficient> + <S_ref Desc="Stabiliser reference area" ToolLevel="1" Unit="m2">32.46074351</S_ref> + </Stabiliser> + <VerticalTail> + <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">0.1018345125</VolumeCoefficient> + <S_ref Desc="Fin reference area" ToolLevel="1" Unit="m2">26.57458461</S_ref> + </VerticalTail> + </StabilityAndControlCharacteristics> + <Performance Desc="Flugleistungen"> + <Range Desc="Reichweiten"> + <Range_maxPayloadatMTOM Desc="Reichweite bei maximaler Nutzlast und Betankung bis zum MTOM-Limit" ToolLevel="2" Unit="km">3043.938845</Range_maxPayloadatMTOM> + <Range_maxFuelatMTOM Desc="Reichweite bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="km">11558.21333</Range_maxFuelatMTOM> + <Payload_maxFuelatMTOM Desc="Payload bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="kg">3895.43595</Payload_maxFuelatMTOM> + <Range_maxFuelEmpty Desc="Ueberfuehrungsreichweite, leer mit vollen Tanks" ToolLevel="2" Unit="km">12572.68487</Range_maxFuelEmpty> + </Range> + <Speed Desc="Fluggeschwindigkeiten"> + <M_initialCruise Desc="Cruisemachzahl" ToolLevel="3" Unit="-">0.78</M_initialCruise> + <M_maxOperating Desc="Max Operating Cruise Machzahl" ToolLevel="2" Unit="-">0.82</M_maxOperating> + <V_maxOperating Desc="Max Operating Speed (Maximale Staudruckgeschwindigkeit CAS/IAS)" ToolLevel="2" Unit="KCAS">350</V_maxOperating> + <M_Dive Desc="Diving Mach Number" ToolLevel="2" Unit="-">0.902</M_Dive> + <V_Dive Desc="Diving Speed" ToolLevel="2" Unit="KCAS">385</V_Dive> + <V_s1g Desc="1-g Stalling Speed" ToolLevel="2" Unit="KCAS">161.952013</V_s1g> + </Speed> + <Altitudes Desc="Flughoehen"> + <h_initialCruise Desc="Reiseflughoehe" ToolLevel="3" Unit="m">10058.4</h_initialCruise> + <h_maxCertified Desc="maximal zugelassene Flughoehe (s. TLAR)" ToolLevel="3" Unit="m">11734.8</h_maxCertified> + <h_maxOperating Desc="Dienstgipfelhoehe (100 ft/min Steigkriterium)" ToolLevel="3" Unit="m">12010.7005</h_maxOperating> + <h_maxCeiling Desc="Maximale Flughoehe (50 ft/min Steigkriterium) bei MTOM" ToolLevel="3" Unit="m">12053.19642</h_maxCeiling> + <h_maxOEI Desc="Maximale Flughoehe (100 ft/min Steigkriterium) bei einem Triebwerksausfall und bei MTOM" ToolLevel="3" Unit="m">7730.61576</h_maxOEI> + </Altitudes> + <Climb Desc="Steigflug"> + <TTC_Design Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA+10)" ToolLevel="3" Unit="min">14.56137643</TTC_Design> + <Time_to_1500ft_ISA10 Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA+10)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA10> + <Time_to_ICA_ISA10 Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="min">15.53402313</Time_to_ICA_ISA10> + <Range_to_ICA_ISA10 Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="NM">89.09881839</Range_to_ICA_ISA10> + <Fuel_to_ICA_ISA10 Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="kg">1577.91233</Fuel_to_ICA_ISA10> + <TTC_ISA Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA)" ToolLevel="3" Unit="min">5.079260451</TTC_ISA> + <Time_to_1500ft_ISA Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA> + <Time_to_ICA_ISA Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="min">6.051907144</Time_to_ICA_ISA> + <Range_to_ICA_ISA Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="NM">22.96381264</Range_to_ICA_ISA> + <Fuel_to_ICA_ISA Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="kg">732.9613247</Fuel_to_ICA_ISA> + <TTC_ISA10_optROC Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">5.079260451</TTC_ISA10_optROC> + <Time_to_1500ft_ISA10_optROC Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA10_optROC> + <Time_to_ICA_ISA10_optROC Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">6.051907144</Time_to_ICA_ISA10_optROC> + <Range_to_ICA_ISA10_optROC Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="NM">22.96381264</Range_to_ICA_ISA10_optROC> + <Fuel_to_ICA_ISA10_optROC Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="kg">732.9613247</Fuel_to_ICA_ISA10_optROC> + </Climb> + <TakeOff Desc="Start Performance"> + <TakeOffDistance_Normal Desc="Startstrecke - Normalstartstrecke bei MTOM und ISA+15" ToolLevel="2" Unit="m">1731.705965</TakeOffDistance_Normal> + <BFL Desc="Startstrecke - Balanced Fieldlength bei MTOM und ISA+15 " ToolLevel="2" Unit="m">1853.411621</BFL> + <TimeToScreenHeight Desc="Zeit bis zum erreichen von 35 ft" ToolLevel="2" Unit="s">34.72221827</TimeToScreenHeight> + <V_LOF Desc="Abhebegeschwindigkeit" ToolLevel="2" Unit="KCAS">136.8991062</V_LOF> + <V_1 Desc="Decision Speed bei fuer MTOM BLFL" ToolLevel="2" Unit="KCAS">135.3462489</V_1> + <V_2 Desc="Geschwindigkeit auf Screen height (35 ft)" ToolLevel="2" Unit="KCAS">136.8991062</V_2> + <V_FTO Desc="Geschwindigkeit am Ende des Final T-O Segment (1500 ft)" ToolLevel="2" Unit="KCAS">203.0413711</V_FTO> + <ScdSegmentClimbGradient Desc="Steigradient im zweiten Steigsegment TO" ToolLevel="2" Unit="%">2.68313876</ScdSegmentClimbGradient> + <FinalSegmentClimbGradient Desc="Steigradient im zweiten Steigsegment TO" ToolLevel="2" Unit="%">2.683126144</FinalSegmentClimbGradient> + </TakeOff> + <Landing> + <LandingDistance Desc="Landestrecke" ToolLevel="2" Unit="m">1528.071526</LandingDistance> + <V_Approach Desc="Anfluggeschwindigkeit" ToolLevel="2" Unit="KCAS">129.2323788</V_Approach> + </Landing> + <MissionAnalysis Desc="Missionsanalyse"> + <DesignMission Desc="Parameter der Design-Mission"> + <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionDesign.xml</MissionFile> + <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">2</CruiseSteps> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">0.5008065466</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">330.0000005</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">18070.1076</Missionfuel> + <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">14883.27019</Tripfuel> + <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">90.32770904</TaxifuelTakeoff> + <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">50.18206058</TaxifuelLdg> + <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">5.947085161</Blocktime> + <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">5.713751827</Flighttime> + <Range Desc="Range" ToolLevel="3" Unit="NM">2500.55303</Range> + <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">76962.57512</TOM> + <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">17000</Payload> + <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX> + <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">3392</CargoMass> + <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate> + <Offtakes> + <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL"> + <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">73.40008433</ShaftPowerTotal> + <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.9793842105</BleedAirTotal> + </AverageCruiseOfftakes> + </Offtakes> + <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug"> + <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.5148367758</CL_avg> + <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4915188994</CL_min> + <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.5675400636</CL_max> + </LiftCoefficientsCruise> + <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs"> + <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">75060.13292</Mass_TOC> + <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">62441.91279</Mass_TOD> + </MassesCruise> + </DesignMission> + <StudyMission Desc="Parameter der Study-Mission"> + <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionStudy.xml</MissionFile> + <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">1</CruiseSteps> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15"> + <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength> + <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel> + </CruiseStep> + <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">5967.411758</Missionfuel> + <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">3241.768614</Tripfuel> + <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">90.32770904</TaxifuelTakeoff> + <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">50.18206058</TaxifuelLdg> + <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">1.50538405</Blocktime> + <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">1.272050716</Flighttime> + <Range Desc="Range" ToolLevel="3" Unit="NM">500.546566</Range> + <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">61467.87928</TOM> + <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">13608</Payload> + <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX> + <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">0</CargoMass> + <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate> + <Offtakes> + <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL"> + <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">72.97412478</ShaftPowerTotal> + <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.9793842105</BleedAirTotal> + </AverageCruiseOfftakes> + </Offtakes> + <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug"> + <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.4681348875</CL_avg> + <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4621586298</CL_min> + <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4991350396</CL_max> + </LiftCoefficientsCruise> + <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs"> + <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">60071.12337</Mass_TOC> + <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">58584.28057</Mass_TOD> + </MassesCruise> + </StudyMission> + </MissionAnalysis> + <RequirementsChecks> + <MissionFile Desc="Dateiname der Missionsdatei" OfftakesWritten="1" ToolLevel="1" Unit="-">missionReq.xml</MissionFile> + <TLARs> + <TOFL_Design Checked="1" ToolLevel="2">1</TOFL_Design> + <LDN_Design Checked="1" ToolLevel="2">1</LDN_Design> + <V_ApproachSpeed_Design Checked="1" ToolLevel="2">1</V_ApproachSpeed_Design> + <h_initialCruise_Design Checked="1" ToolLevel="3">1</h_initialCruise_Design> + <h_maxOperating Checked="1" ToolLevel="3">1</h_maxOperating> + <h_maxOEI Checked="1" ToolLevel="3">1</h_maxOEI> + <M_initialCruise_Design Checked="1" ToolLevel="3">1</M_initialCruise_Design> + <TTC_Design Checked="1" ToolLevel="3">1</TTC_Design> + </TLARs> + <Certification> + <climbGradientSecondTOSegment Checked="1" ToolLevel="2">1</climbGradientSecondTOSegment> + <climbGradientFinalTOSegment Checked="1" ToolLevel="2">1</climbGradientFinalTOSegment> + <climbGradientApproachOEI Checked="1" ToolLevel="2">1</climbGradientApproachOEI> + <climbGradientApproachAEO Checked="1" ToolLevel="2">1</climbGradientApproachAEO> + </Certification> + </RequirementsChecks> + </Performance> + <MonetaryValues Desc="Kosten und Preise"> + <MonetaryScenario> + <AirframeEngineeringHours Desc="Anzahl der Arbeitsstunden in der FZ-Entwicklung" ToolLevel="1" Unit="h">12079799</AirframeEngineeringHours> + <ProductionVolume Desc="Anzahl produzierter Flugzeuge je Programm" ToolLevel="1">1500</ProductionVolume> + </MonetaryScenario> + <Earnings Desc="Herstellergewinn pro verkauftem Flugzeug" ToolLevel="1" Unit="$">28158406</Earnings> + <NPV Desc="Net Present Value (Kapitalwert) fuer Flugzeugprogramm bei Verkauf des gesamten ProductionVolume" ToolLevel="1" Unit="Mio.$">33855.557</NPV> + <Prices Desc="Preise"> + <PriceAirplane Desc="airplane price (for the whole plane); for the insurance and for the Simple_deprecition in DOC-Tool" ToolLevel="1" Unit="$">71228241.8</PriceAirplane> + <DiscountRate Desc="discount rate on airplane lst price granted airlines" ToolLevel="1" Unit="-">0.07</DiscountRate> + </Prices> + <LCC Desc="Life Cycle Costs"> + <NonRecurringCosts Desc="Non-Recurring Costs fuer gesamtes Flugzeugprogramm"> + <NRCTotal Desc="Non Recurring Costs" ToolLevel="1" Unit="$">3475793421</NRCTotal> + <NRCComponents> + <AirframeEngAndDesign Desc="Costs for Airframe Engineering and Design" ToolLevel="1" Unit="$">1359777460</AirframeEngAndDesign> + <DevSupportAndTesting Desc="Costs for Development Support and Testing" ToolLevel="1" Unit="$">345988343</DevSupportAndTesting> + <FlightTestAC> + <FlightTestACTotal Desc="Costs for Flight Test Aircraft" ToolLevel="1" Unit="$">1636269510</FlightTestACTotal> + <FlightTestACComponents> + <EngineAndAvionics Desc="Costs for Engines and Avionics" ToolLevel="1" Unit="$">117031730</EngineAndAvionics> + <LaborManufacturing Desc="Costs for Manufacturing Labor" ToolLevel="1" Unit="$">622590665</LaborManufacturing> + <MaterialManufacturing Desc="Costs for Manufacturing Material" ToolLevel="1" Unit="$">188900611</MaterialManufacturing> + <Tooling Desc="Costs for Tooling" ToolLevel="1" Unit="$">624941946</Tooling> + <QualityControl Desc="Costs for Quality Control" ToolLevel="1" Unit="$">82804558</QualityControl> + </FlightTestACComponents> + </FlightTestAC> + <FlightTestOp Desc="Costs for Flight Test Operations" ToolLevel="1" Unit="$">133758109</FlightTestOp> + <Facilities Desc="Costs for Test and Simulation Facilities" ToolLevel="1" Unit="$">0</Facilities> + </NRCComponents> + </NonRecurringCosts> + <RecurringCosts Desc="Recurring Costs"> + <RCTotal Desc="Recurring Costs" ToolLevel="1" Unit="$">35766663</RCTotal> + <RCComponents> + <Wing Desc="Costs for Wing" ToolLevel="1" Unit="$">2408072</Wing> + <Fuselage Desc="Costs for Fuselage" ToolLevel="1" Unit="$">2957731</Fuselage> + <Empennage Desc="Costs for Empennage" ToolLevel="1" Unit="$">584113</Empennage> + <LandingGear Desc="Costs for Landing Gear" ToolLevel="1" Unit="$">639568</LandingGear> + <Pylons Desc="Costs for Pylons" ToolLevel="1" Unit="$">879551</Pylons> + <PowerUnit Desc="Costs for all installed engines with systems without pylons"> + <PowerUnitTotal Desc="Costs for PowerUnit" ToolLevel="1" Unit="$">13337566</PowerUnitTotal> + <PowerUnitComponents> + <EquippedEngines Desc="Costs for Engines Dry and Other Systems" ToolLevel="1" Unit="$">11357394</EquippedEngines> + <Nacelles Desc="Costs for Nacelles" ToolLevel="1" Unit="$">1791842</Nacelles> + <BleedAirSystem Desc="Costs for BleedAirSystem (Airbus Chapter 21, ATA36)" ToolLevel="1" Unit="$">107416</BleedAirSystem> + <FuelSystem Desc="Costs for Fuel System (Airbus Chapter 23, ATA28)" ToolLevel="1" Unit="$">80914</FuelSystem> + </PowerUnitComponents> + </PowerUnit> + <Systems> + <SystemsTotal Desc="Costs for Systems" ToolLevel="1" Unit="$">7436254</SystemsTotal> + <SystemsComponents> + <APU Desc="Costs for APU (Airbus Chapter 30, ATA49)" ToolLevel="1" Unit="$">273442</APU> + <HydraulicSystem Desc="Costs for Hydraulic System (Airbus Chapter 31 + 32,ATA29)" ToolLevel="1" Unit="$">220982</HydraulicSystem> + <AirConditioning Desc="Costs for Air Conditioning (Airbus Chapter 33, ATA21)" ToolLevel="1" Unit="$">694499</AirConditioning> + <DeIcing Desc="Costs for De-Icing (Airbus Chapter 34, ATA30)" ToolLevel="1" Unit="$">40295</DeIcing> + <FireProtection Desc="Costs for Fire Protection (Airbus Chapter 35, ATA26)" ToolLevel="1" Unit="$">39314</FireProtection> + <FlightControls Desc="Costs for Flight Controls (Airbus Chapter 36, ATA27)" ToolLevel="1" Unit="$">598096</FlightControls> + <Instruments Desc="Costs for Instruments (Airbus Chapter 37, ATA31)" ToolLevel="1" Unit="$">343899</Instruments> + <AutomaticFlightSystem Desc="Costs for Automatic Flight System (Airbus Chapter 38, ATA22)" ToolLevel="1" Unit="$">558835</AutomaticFlightSystem> + <Navigation Desc="Costs for Navigation (Airbus Chapter 39, ATA34)" ToolLevel="1" Unit="$">2278329</Navigation> + <Communication Desc="Costs for Communication (Airbus Chapter 40, ATA23)" ToolLevel="1" Unit="$">1117671</Communication> + <ElectricalSystem Desc="Costs for Air Conditioning (Airbus Chapter 41+42, ATA24)" ToolLevel="1" Unit="$">1270893</ElectricalSystem> + </SystemsComponents> + </Systems> + <Furnishings> + <FurnishingsTotal Desc="Costs for Furnishings" ToolLevel="1" Unit="$">1442699</FurnishingsTotal> + <FurnishingsComponents> + <Furnishing Desc="Costs for Furnishings (Airbus Chapter 50, ATA25)" ToolLevel="1" Unit="$">1048900</Furnishing> + <FixedEmergencyOxygen Desc="Costs for Fixed Emergency Oxygen (Airbus Chapter 51, ATA35)" ToolLevel="1" Unit="$">41911</FixedEmergencyOxygen> + <Lighting Desc="Costs for Lighting (Airbus Chapter 52, ATA33)" ToolLevel="1" Unit="$">228444</Lighting> + <WaterInstallation Desc="Costs for Water Installation (Airbus Chapter 53, ATA38)" ToolLevel="1" Unit="$">123443</WaterInstallation> + </FurnishingsComponents> + </Furnishings> + <OperatorsItems Desc="Costs for OperatorItems (Airbus Chapter 60+61)" ToolLevel="1" Unit="$">1415894</OperatorsItems> + <FinalAssembly Desc="Costs for FinalAssembly" ToolLevel="1" Unit="$">4665217</FinalAssembly> + </RCComponents> + </RecurringCosts> + <OperatingCosts> + <OperatingScenario Desc="Umrechnungsfaktor fuer verschiedene DOC-Einheiten, zusaetzlich aus A/C-XML: Nseats=PassengersTotal"> + <FlightsPerYear Desc="Flights per year / take-offs annually; aus operating_company.xml" ToolLevel="1" Unit="">2230</FlightsPerYear> + <SeatLoadFactor Desc="utilisation factor for the payload; aus operating_company.xml" ToolLevel="1" Unit="">1</SeatLoadFactor> + </OperatingScenario> + <DirectOperatingCosts> + <DOC_total Desc="Summe aller DOCComponents (s.u)"> + <DOC_year Desc="DOC pro Jahr" ToolLevel="1" Unit="$/year">20437514.98</DOC_year> + <DOC_FH Desc="DOC pro Flugstunde = DOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">7204.76</DOC_FH> + <DOC_flight Desc="DOC pro Flug = DOC_year/(Nta)" ToolLevel="1" Unit="$/flight">9164.81</DOC_flight> + <DOC_km Desc="DOC pro km = DOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">9.9</DOC_km> + <DOC_100ASK Desc="DOC pro 100 Available Seat Kilometer = DOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">6.6</DOC_100ASK> + </DOC_total> + <COC_total Desc="Summe aller DOCComponents ausser Depreciation und Insurance"> + <COC_year Desc="COC pro Jahr" ToolLevel="1" Unit="$/year">17054173.5</COC_year> + <COC_FH Desc="COC pro Flugstunde = COC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">6012.05</COC_FH> + <COC_flight Desc="COC pro Flug = COC_year/(Nta)" ToolLevel="1" Unit="$/flight">7647.62</COC_flight> + <COC_km Desc="COC pro km = COC_year/(Nta*R)" ToolLevel="1" Unit="$/km">8.26</COC_km> + <COC_100ASK Desc="COC pro 100 Available Seat Kilometer = COC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">5.50770807</COC_100ASK> + </COC_total> + <DOCComponents Desc="DOC-Anteile in 100ASK"> + <Charge Desc="Gebuehren pro 100ASK"> + <ChargeTotal Desc="total charges" ToolLevel="1" Unit="$/100ASK">1.83</ChargeTotal> + <ChargesComponents> + <NavigationCharge Desc="navigational charges" ToolLevel="1" Unit="$/100ASK">0.73</NavigationCharge> + <LandingCharge Desc="landing charges" ToolLevel="1" Unit="$/100ASK">0.33</LandingCharge> + <LandingChargeComponents> + <NoiseCharge Desc="noise charges" ToolLevel="1" Unit="$/100ASK">0</NoiseCharge> + <NOxCharge Desc="NOx charges" ToolLevel="1" Unit="$/100ASK">0</NOxCharge> + <ChargeWithoutEmission Desc="landing charges without emissions (noise + NOx)" ToolLevel="1" Unit="$/100ASK">0.33</ChargeWithoutEmission> + </LandingChargeComponents> + <GroundCharge Desc="ground charges" ToolLevel="1" Unit="$/100ASK">0.77</GroundCharge> + </ChargesComponents> + </Charge> + <Depreciation Desc="Abschreibungskosten" ToolLevel="1" Unit="$/100ASK">0.98</Depreciation> + <Insurance Desc="Versicherungskosten" ToolLevel="1" Unit="$/100ASK">0.11</Insurance> + <Maintenance Desc="Wartungskosten"> + <MaintenanceTotal Desc="Wartungskosten gesamt" ToolLevel="1" Unit="$/100ASK">0.75</MaintenanceTotal> + <MaintenanceComponents> + <Airframe Desc="Wartungskosten Airframe"> + <AirframeTotal Desc="Wartungskosten Airframe gesamt" ToolLevel="1" Unit="$/100ASK">0.3</AirframeTotal> + <CostComponents> + <LabourCosts Desc="Arbeitskosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0.243</LabourCosts> + <MaterialCosts Desc="Materialkosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0.061</MaterialCosts> + </CostComponents> + <AirframeComponents Desc="Kostenwert fuer das ATA Kapitel"> + <ATA21 Desc="Environmental Control System"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0134</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0107</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0027</MaterialCosts> + </CostComponents> + </ATA21> + <ATA22 Desc="Autoflight"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0127</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0102</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0025</MaterialCosts> + </CostComponents> + </ATA22> + <ATA23 Desc="Communications"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0123</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0098</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0025</MaterialCosts> + </CostComponents> + </ATA23> + <ATA24 Desc="Electrical System"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0211</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0169</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0042</MaterialCosts> + </CostComponents> + </ATA24> + <ATA25 Desc="Furnishing"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0409</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0327</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0082</MaterialCosts> + </CostComponents> + </ATA25> + <ATA26 Desc="Fire Protection"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0043</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0035</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0009</MaterialCosts> + </CostComponents> + </ATA26> + <ATA27 Desc="Flight Control System"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.025</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.02</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.005</MaterialCosts> + </CostComponents> + </ATA27> + <ATA28 Desc="Fuel System"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0022</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0018</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0004</MaterialCosts> + </CostComponents> + </ATA28> + <ATA29 Desc="Hydraulic System"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0131</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0105</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0026</MaterialCosts> + </CostComponents> + </ATA29> + <ATA30 Desc="Ice and Rain Protection"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0015</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0012</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0003</MaterialCosts> + </CostComponents> + </ATA30> + <ATA31 Desc="Instrumentation"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0016</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0013</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0003</MaterialCosts> + </CostComponents> + </ATA31> + <ATA32 Desc="Landing Gear"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0559</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0447</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0112</MaterialCosts> + </CostComponents> + </ATA32> + <ATA33 Desc="Lights"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0051</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0041</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.001</MaterialCosts> + </CostComponents> + </ATA33> + <ATA34 Desc="Navigation"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0142</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0113</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0028</MaterialCosts> + </CostComponents> + </ATA34> + <ATA35 Desc="Oxygen"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.003</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0024</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0006</MaterialCosts> + </CostComponents> + </ATA35> + <ATA36 Desc="Pneumatic"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0036</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0029</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0007</MaterialCosts> + </CostComponents> + </ATA36> + <ATA38 Desc="Water and Waste"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0024</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0019</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0005</MaterialCosts> + </CostComponents> + </ATA38> + <ATA49 Desc="APU"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0104</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0083</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0021</MaterialCosts> + </CostComponents> + </ATA49> + <ATA51 Desc="Structure"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.004</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0032</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0008</MaterialCosts> + </CostComponents> + </ATA51> + <ATA52 Desc="Doors"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0054</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0044</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts> + </CostComponents> + </ATA52> + <ATA53 Desc="Fuselage"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0057</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0045</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts> + </CostComponents> + </ATA53> + <ATA54 Desc="Nacelles"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0012</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.001</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0002</MaterialCosts> + </CostComponents> + </ATA54> + <ATA55 Desc="Stabilizers"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0018</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0015</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0004</MaterialCosts> + </CostComponents> + </ATA55> + <ATA56 Desc="Windows"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0081</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0065</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0016</MaterialCosts> + </CostComponents> + </ATA56> + <ATA57 Desc="Wings"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0056</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0045</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts> + </CostComponents> + </ATA57> + <ATA99 Desc="Routinearbeiten, hauptsaechlich Inspektion"> + <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0294</TotalCosts> + <CostComponents> + <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0235</LabourCosts> + <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0059</MaterialCosts> + </CostComponents> + </ATA99> + </AirframeComponents> + </Airframe> + <Engine Desc="Wartungskosten Triebwerk" ToolLevel="1" Unit="$/100ASK">0.45</Engine> + </MaintenanceComponents> + </Maintenance> + <Fuel Desc="Spritkosten" ToolLevel="1" Unit="$/100ASK">2.44</Fuel> + <Crew Desc="Crew Kosten"> + <CrewTotal Desc="Crew Kosten gesamt" ToolLevel="1" Unit="$/100ASK">0.49</CrewTotal> + <CrewComponents> + <FlightCrew Desc="Flight Crew Kosten" ToolLevel="1" Unit="$/100ASK">0.12</FlightCrew> + <CabinCrew Desc="Cabin Crew Kosten" ToolLevel="1" Unit="$/100ASK">0.36</CabinCrew> + </CrewComponents> + </Crew> + <Delay Desc="Verspaetungskosten" ToolLevel="1" Unit="$/100ASK">0</Delay> + </DOCComponents> + </DirectOperatingCosts> + <IndirectOperatingCosts> + <IOC_total Desc="Summe aller IOCComponents (s.u)"> + <IOC_year Desc="IOC pro Jahr" ToolLevel="1" Unit="$/year">20699680.51</IOC_year> + <IOC_FH Desc="IOC pro Flugstunde = IOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">7297.17</IOC_FH> + <IOC_flight Desc="IOC pro Flug = IOC_year/(Nta)" ToolLevel="1" Unit="$/flight">9282.37</IOC_flight> + <IOC_km Desc="IOC pro km = IOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">10.02</IOC_km> + <IOC_100ASK Desc="IOC pro 100 Available Seat Kilometer = IOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">6.68</IOC_100ASK> + </IOC_total> + </IndirectOperatingCosts> + </OperatingCosts> + <EndOfLifeCosts> + <EOLCTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="$">48616</EOLCTotal> + <EOLCTotalComponents> + <TransportToEoLSite Desc="Kosten fuer Transport zur Abwrack-Location" ToolLevel="1" Unit="$">9140</TransportToEoLSite> + <DisassemblyAndDismantling Desc="Kosten fuer Dissassembly and Dismantling" ToolLevel="1" Unit="$">124837</DisassemblyAndDismantling> + <Recycling Desc="Materialrecycling, bei negativem Wert Benefit durch Materialverkauf" ToolLevel="1" Unit="$">-86485</Recycling> + <Incineration Desc="Kosten fuer Verbrennung (inkl. shredding, mixing, incineration, and landfill of ash) " ToolLevel="1" Unit="$">297</Incineration> + <Landfill Desc="Kosten fuer Landfill" ToolLevel="1" Unit="$">827</Landfill> + </EOLCTotalComponents> + </EndOfLifeCosts> + </LCC> + </MonetaryValues> + <EcologicalValues Desc="Oekologische Bewertung"> + <Noise Desc="Akustische Kenngroessen und Laermbewertungsmasse"> + <NoisePathFiles> + <Departure Desc="Dateiname des Departure Path" ToolLevel="1">0</Departure> + <Approach Desc="Dateiname des Approach Path" ToolLevel="1">0</Approach> + </NoisePathFiles> + <NoiseCertificationLevels> + <LateralPoint> + <LateralFullPower Desc="EPNL Sideline Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</LateralFullPower> + <SPL Desc="dBA at lateral point" ToolLevel="1" Unit="dBA">0</SPL> + <Loudness Desc="Loudness at lateral point" ToolLevel="1" Unit="Sone">0</Loudness> + <Tonality Desc="Tonality at lateral point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality> + <Sharpness Desc="Sharpness at lateral point" ToolLevel="1" Unit="Acum">0</Sharpness> + <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at lateral point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance> + </LateralPoint> + <FlyoverPoint> + <Flyover Desc="EPNL Flyover Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Flyover> + <SPL Desc="dBA at flyover point" ToolLevel="1" Unit="dBA">0</SPL> + <Loudness Desc="Loudness at flyover point" ToolLevel="1" Unit="Sone">0</Loudness> + <Tonality Desc="Tonality at flyover point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality> + <Sharpness Desc="Sharpness at flyover point" ToolLevel="1" Unit="Acum">0</Sharpness> + <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at flyover point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance> + </FlyoverPoint> + <ApproachPoint> + <Approach Desc="EPNL Approach Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Approach> + <SPL Desc="dBA at approach point" ToolLevel="1" Unit="dBA">0</SPL> + <Loudness Desc="Loudness at approach point" ToolLevel="1" Unit="Sone">0</Loudness> + <Tonality Desc="Tonality at approach point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality> + <Sharpness Desc="Sharpness at approach point" ToolLevel="1" Unit="Acum">0</Sharpness> + <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at approach point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance> + </ApproachPoint> + <CumulativeValues> + <EPNdB Desc="EPNL Cumulative Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</EPNdB> + <SPL Desc="Cumulative dBA at the three points" ToolLevel="1" Unit="dBA">0</SPL> + <Loudness Desc="Cumulative Loudness at the three points" ToolLevel="1" Unit="Sone">0</Loudness> + <Tonality Desc="Tonality at the three points" ToolLevel="1" Unit="tonality units t.u.">0</Tonality> + <Sharpness Desc="Sharpness at the three points" ToolLevel="1" Unit="Acum">0</Sharpness> + <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at the three points" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance> + </CumulativeValues> + </NoiseCertificationLevels> + <CommunityNoiseLevels> + <TakeOff> + <SPL Desc="Sound Pressure Level 10km from brake release" ToolLevel="1" Unit="dBA">0</SPL> + <SPLarea> + <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1> + <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2> + </SPLarea> + <PNLarea> + <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1> + <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2> + </PNLarea> + <PNLTarea> + <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1> + <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2> + </PNLTarea> + <EPNLarea> + <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1> + <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2> + </EPNLarea> + <LoudnessArea> + <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold1> + <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold2> + </LoudnessArea> + <TonalityArea> + <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1> + <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.15 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2> + <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3> + <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.35 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4> + </TonalityArea> + <SharpnessArea> + <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1> + <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2> + </SharpnessArea> + <PsychoacousticAnnoyanceArea> + <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1> + <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2> + </PsychoacousticAnnoyanceArea> + <SELarea Desc="Sound Exposure Level area"> + <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85> + <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75> + <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65> + <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55> + </SELarea> + </TakeOff> + <Approach> + <SPL Desc="Sound Pressure Level 15km from touchdown" ToolLevel="1" Unit="dBA">0</SPL> + <SPLarea> + <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1> + <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2> + </SPLarea> + <PNLarea> + <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1> + <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2> + </PNLarea> + <PNLTarea> + <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1> + <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2> + </PNLTarea> + <EPNLarea> + <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1> + <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2> + </EPNLarea> + <LoudnessArea> + <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold1> + <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold2> + </LoudnessArea> + <TonalityArea> + <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1> + <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.10 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2> + <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.20 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3> + <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4> + </TonalityArea> + <SharpnessArea> + <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1> + <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2> + </SharpnessArea> + <PsychoacousticAnnoyanceArea> + <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1> + <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2> + </PsychoacousticAnnoyanceArea> + <SELarea Desc="Sound Exposure Level area"> + <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85> + <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75> + <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65> + <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55> + </SELarea> + </Approach> + <CumulativeValues> + <EPNdB Desc="85 EPNdB area sum for takeoff and approach" ToolLevel="1" Unit="EPNdB">0</EPNdB> + <SPL Desc="75 dBA area sum for takeoff and approach" ToolLevel="1" Unit="dBA">0</SPL> + <Loudness Desc="85 Phon loudness area sum for takeoff and approach" ToolLevel="1" Unit="Sone">0</Loudness> + <Tonality Desc="Tonality area sum for takeoff and approach - 0.1 t.u. for short-range and 0.2 t.u. for long-range AC" ToolLevel="1" Unit="tonality units t.u.">0</Tonality> + <Sharpness Desc="1.0 Acum sharpness area sum for takeoff and approach" ToolLevel="1" Unit="Acum">0</Sharpness> + <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance of 10 area sum for takeoff and approach" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance> + </CumulativeValues> + </CommunityNoiseLevels> + </Noise> + <Emissions> + <Development Desc="Analyse der Entwicklungsphase fuer gesamtes Flugzeugprogramm"> + <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">11763648.53</CO2> + <H2O Desc="Wasser" ToolLevel="1" Unit="kg">40697548.71</H2O> + <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">22681.579</NOx> + <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">506.978</CO> + <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">10059.553</SO2> + <CH4 Desc="Methan" ToolLevel="1" Unit="kg">16890.095</CH4> + <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">176.255</PM10> + <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">982.444</N2O> + <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0.019</PFC> + <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">1432.078</NMVOC> + <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-4663.364</HC> + </Development> + <Production> + <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">618228.677</CO2> + <H2O Desc="Wasser" ToolLevel="1" Unit="kg">5361791.97</H2O> + <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">1320.026</NOx> + <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">1715.593</CO> + <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">2280.541</SO2> + <CH4 Desc="Methan" ToolLevel="1" Unit="kg">1327.591</CH4> + <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">5.711</PM10> + <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O> + <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC> + <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC> + <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-5.298</HC> + </Production> + <Operations> + <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">649479288.1</CO2> + <H2O Desc="Wasser" ToolLevel="1" Unit="kg">269362047.2</H2O> + <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">821056.648</NOx> + <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">279870.45</CO> + <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">533623.487</SO2> + <CH4 Desc="Methan" ToolLevel="1" Unit="kg">749253.374</CH4> + <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">10631.577</PM10> + <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O> + <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC> + <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC> + <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-247022.508</HC> + <OperationComponents> + <ICAO_LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle gemaess ICAO Engine Emission Database und Standardzeiten fuer eine (!) StudyMission"> + <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">2844.948</CO2> + <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">1084.134</H2O> + <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.759</SO2> + <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">99.106</HC> + <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">5.747</CO> + <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">11.071</NOx> + <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.023</PM10> + </ICAO_LTO> + <Mission Desc="Environmental analysis of one study mission"> + <LTOTimes Desc="Times of LTO phases (all phases under 3000 ft)"> + <Total Desc="Taxi, Take-off, Climb Out and Approach time (LTO)" ToolLevel="1" Unit="min">19.622</Total> + <TaxiTime Desc="Time for taxi (ICAO: 26 min)" ToolLevel="1" Unit="min">14</TaxiTime> + <TakeOffTime Desc="Time for take-off (until 35ft) (ICAO: 0.7 min)" ToolLevel="1" Unit="min">0.311</TakeOffTime> + <ClimbOutTime Desc="Time for climb out (35 ft to 3000ft)(ICAO: 2.2 min)" ToolLevel="1" Unit="min">0.933</ClimbOutTime> + <ApproachTime Desc="Time for approach (from 3000 ft to stop)(ICAO: 4 min)" ToolLevel="1" Unit="min">4.377</ApproachTime> + </LTOTimes> + <LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle mit Missionsanalyse fuer eine (!) StudyMission"> + <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">1500.242</CO2> + <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">571.702</H2O> + <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.4</SO2> + <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">-2.376</HC> + <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">2.018</CO> + <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">3.831</NOx> + <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.009</PM10> + </LTO> + <Cruise Desc="Triebwerksemissionen des Reiseflugs fuer eine (!) StudyMission"> + <CO2 Desc="CO2 emitted during cruise" ToolLevel="1" Unit="kg">9149.073</CO2> + <H2O Desc="H2O emitted during cruise" ToolLevel="1" Unit="kg">3486.468</H2O> + <SO2 Desc="SO2 emitted during cruise" ToolLevel="1" Unit="kg">2.441</SO2> + <HC Desc="HC emitted during cruise" ToolLevel="1" Unit="kg">-2.055</HC> + <CO Desc="CO emitted during cruise" ToolLevel="1" Unit="kg">1.349</CO> + <NOx Desc="NOx emitted during cruise" ToolLevel="1" Unit="kg">7.688</NOx> + <PM10 Desc="PM10 emitted during cruise" ToolLevel="1" Unit="kg">0.01</PM10> + </Cruise> + </Mission> + </OperationComponents> + </Operations> + <EndOfLife> + <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">-114694.14</CO2> + <H2O Desc="Wasser" ToolLevel="1" Unit="kg">-1466106.754</H2O> + <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">-495.854</NOx> + <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">-1949.608</CO> + <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">-1061.466</SO2> + <CH4 Desc="Methan" ToolLevel="1" Unit="kg">-304.18</CH4> + <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0.419</PM10> + <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O> + <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC> + <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC> + <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-3.735</HC> + </EndOfLife> + </Emissions> + <CED Desc="Cumulative Energy Demand"> + <CEDTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="MJ">1.033604491e+16</CEDTotal> + <CEDComponents> + <Development Desc="Development" ToolLevel="1" Unit="MJ">2.115958924e+14</Development> + <Production Desc="Production" ToolLevel="1" Unit="MJ">1.332765215e+13</Production> + <Operations Desc="Operation" ToolLevel="1" Unit="MJ">1.011292433e+16</Operations> + <EndOfLife Desc="End of Life" ToolLevel="1" Unit="MJ">-1.802957726e+12</EndOfLife> + </CEDComponents> + </CED> + <ClimateImpact Desc="Climate Impact due to Aircraft Operation"> + <ATR Desc="Average Temperatur Response per year for aircraft operating lifetime" ToolLevel="1" Unit="mK">0.0014420111</ATR> + <AGTP Desc="Absolute Global Temperature Potential after final year of operation" ToolLevel="1" Unit="K">2.13271e-05</AGTP> + <AGTP100 Desc="Absolute Global Temperature Potential after 100 years" ToolLevel="1" Unit="K">3.52252e-05</AGTP100> + <AGWP Desc="Absolute Global Warming Potential after final year of operation" ToolLevel="1" Unit="(W/m2)*year">4.29914e-05</AGWP> + <AGWP100 Desc="Absolute Global Warming Potential after 100 years" ToolLevel="1" Unit="(W/m2)*year">0</AGWP100> + </ClimateImpact> + <AirQuality Desc="Climate Impact due to Aircraft Operation"> + <ToleranceFactors Desc="Tolerance Factors of Emissions emitted during LTO" Unit="-"> + <HC Desc="TF Kohlenwasserstoff" ToolLevel="1" Unit="-">-0.4355</HC> + <CO Desc="TF Kohlenmonoxid" ToolLevel="1" Unit="-">0.0614</CO> + <NOx Desc="TF Stickoxide" ToolLevel="1" Unit="-">0.1915</NOx> + <soot Desc="TF Russ" ToolLevel="1" Unit="-">0.0767</soot> + </ToleranceFactors> + <AirQualityIndex Desc="Air Quality Index" ToolLevel="1" Unit="-">-0.0265</AirQualityIndex> + </AirQuality> + </EcologicalValues> + <Requirements Desc="Designforderungen"> + <m_Payload Desc="Design-Nutzlast (z.B. Anzahl PAX*MassPerPAX, s. DesignSpecification/Accommodation/)" Unit="kg">17000</m_Payload> + <m_MaximumPayload Desc="Maximale Nutzlast i. a. (PAX + 2*Luggage, da Cargo ~ Luggage)" Unit="kg">20000</m_MaximumPayload> + <DesignMission Desc="Definition der Auslegungsmission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke"> + <R_Design Desc="Auslegungsreichweite" Unit="NM">2500</R_Design> + <TOFL_Design Desc="Auslegungsstartstrecke (Balanced Field Length)" Unit="m">2200</TOFL_Design> + <TTC_Design Desc="Auslegungs- Time-to-Climb (von 1500 ft auf ICA bei ISA+10)" Unit="min">35</TTC_Design> + <ClimbGradients Desc="Steiggradientenforderungen"> + <secondTOsegment Desc="Climb gradient in 2nd take-off segment" Unit="percent">2.4</secondTOsegment> + <finalTOsegment Desc="Climb gradient in final take-off segment" Unit="percent">1.2</finalTOsegment> + <approachAEO Desc="Approach gradient with all engine operating" Unit="percent">3.2</approachAEO> + <approachOEI Desc="Approach gradient with one engine inoperative" Unit="percent">2.1</approachOEI> + </ClimbGradients> + <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop)."> + <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds> + <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit> + <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS> + <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise> + </ClimbSpeedSchedule> + <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude."> + <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit> + <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS> + </DescentSpeedSchedule> + <h_initialCruise_Design Desc="Erste Cruise-Altitude (TOC)" Unit="ft">33000</h_initialCruise_Design> + <M_initialCruise_Design Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise_Design> + <LDN_Design Desc="Auslegungslandestrecke (Sicherheitslandestrecke)" Unit="m">1850</LDN_Design> + <V_ApproachSpeed_Design Desc="Auslegungsanfluggeschwindigkeit in KCAS, Approach Category A: 0-90 kts, B: 91-120 kts, C: 121-140 kts, D: 141-165 kts, E: greater 165 kts" Unit="KCAS">138</V_ApproachSpeed_Design> + <AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance> + <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure> + <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure> + <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin> + <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination> + </DesignMission> + <StudyMission Desc="Definition der Study-Mission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke"> + <R_Design Desc="Auslegungsreichweite" Unit="NM">500</R_Design> + <m_Payload Desc="Nutzlast auf Study-Mission" Unit="kg">13608</m_Payload> + <NumberOfPAX Desc="Anzahl Passagiere auf Study-Mission" Unit="-">150</NumberOfPAX> + <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop)."> + <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds> + <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit> + <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS> + <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise> + </ClimbSpeedSchedule> + <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude."> + <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit> + <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS> + </DescentSpeedSchedule> + <h_initialCruise Desc="Erste Cruise-Altitude (TOC)" Unit="ft">35000</h_initialCruise> + <M_initialCruise Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise> + <AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance> + <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure> + <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure> + <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin> + <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination> + </StudyMission> + <FuelPlanningMethod Desc="Methode zur Tankschaetzung: JAR, FAR-Domestic, FAR-Flag (International)">JAR</FuelPlanningMethod> + <V_MaximumGroundspeed Desc="Maximale Rollgeschwindigkeit, durch das Tyre Speed Rating begrenzt in KCAS" Unit="KCAS">195</V_MaximumGroundspeed> + <DesignFlightEnvelope> + <VMO Desc="Max operating speed. IAS also die Strukturbestimmenden Staudruckgeschwindigkeit" Unit="KCAS">350</VMO> + <MMO Desc="Max operating Mach No." Unit="-">0.82</MMO> + <h_maxOperating Desc="Max operating Altitude" Unit="ft">38500</h_maxOperating> + <h_maxOEI Desc="Max operating Altitude One-Engine-Inoperative" Unit="ft">15000</h_maxOEI> + </DesignFlightEnvelope> + <SizeLimits Desc="maximale geometrische Abmasse"> + <SpanLimit Desc="Spannweitenbegrenzung" Unit="m">36</SpanLimit> + </SizeLimits> + <ACN Desc="Aircraft Classification Number"> + <ACNCatType Desc="ACN Pavement Type; flex oder rigid" Unit="-">flex</ACNCatType> + <ACNCategory Desc="ACN Pavement Strength; A, B, C oder D" Unit="-">B</ACNCategory> + <ACNLimit Desc="ACN Limit fuer die ausgewaehlte Kategorie" Unit="-">42</ACNLimit> + </ACN> + </Requirements> + <DesignSpecification Desc="Spezifikation des Entwurfs"> + <Configuration Desc="Qualitative Beschreibung der Konfiguration"> + <Wing Desc="Parameter des Fluegels"> + <Position Desc="Fluegellage low, mid, high" Unit="-">low</Position> + </Wing> + <Stabiliser Desc="Parameter des Hoehenleitwerks"> + <h_OverWing Desc="Vertikale Position bzgl. des Seitenleitwerks (0: conventional 1: T-Tail)" Unit="-">0</h_OverWing> + </Stabiliser> + <LandingGear Desc="Fahrwerksanordnung"> + <MainGearPosition Desc="Position des Hauptfahrwerks (Wing oder Fuselage)">Wing</MainGearPosition> + <Retractable Desc="Switch for (non-)retractable LandingGear">1</Retractable> + </LandingGear> + <Fuselage Desc="Fuselage parameters"> + <Pressurized Desc="Is the fuselage pressurized? 1 for yes, 0 for no">1</Pressurized> + </Fuselage> + <CertificationType Desc="Zertifizierung nach CS-23 oder CS-25">CS-25</CertificationType> + <Fin Desc="Parameter des Seitenleitwerks"> + <FinConfig Desc="0: Conventional 1: H-Tail" Unit="-">0</FinConfig> + </Fin> + </Configuration> + <Accommodation Desc="Vorgaben bezueglich der Passagierdecks und Klassen"> + <MassPerPAX Desc="Masse pro PAX (z.B. PAX 75 kg + Luggage: Std.-Wert 90.72 kg (Quelle Airbus: All about the A320 family, Tech App.))" Unit="kg">90.72</MassPerPAX> + <PAXDecks Desc="Anzahl der Passagierdecks">1</PAXDecks> + <PAXDeck Desc="Passagierdeck mit Klassen in der Folge der Klassen-ID" ID="1"> + <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck">2</Classes> + <Class Desc="Definition der Klasse" ID="1"> + <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">business</ClassType> + <Seating Desc="Bestuhlung des Querschnitts">22</Seating> + <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">12</Seats> + </Class> + <Class Desc="Definition der Klasse" ID="2"> + <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">economy</ClassType> + <Seating Desc="Bestuhlung des Querschnitts">33</Seating> + <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">138</Seats> + </Class> + <Class Desc="Definition der Klasse" ID="3"> + <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">first</ClassType> + <Seating Desc="Bestuhlung des Querschnitts">22</Seating> + <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">0</Seats> + </Class> + </PAXDeck> + </Accommodation> + <Cargo Desc="Vorgaben bezueglich der Frachtdecks und ULDs"> + <CargoDecks Desc="Anzahl der Frachtdecks">1</CargoDecks> + <CargoDeck Desc="Cargodeck mit verschiedenen Containertypen" ID="1"> + <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck">2</Compartments> + <Compartment Desc="Definition des Compartments" ID="1"> + <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">forward</CompartmentType> + <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes> + <ULDType Desc="Definition der Containergruppe" ID="1"> + <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD> + <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow> + <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">3</ULDs> + </ULDType> + </Compartment> + <Compartment Desc="Definition des Compartments" ID="2"> + <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">aft</CompartmentType> + <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes> + <ULDType Desc="Definition der Containergruppe" ID="1"> + <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD> + <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow> + <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">4</ULDs> + </ULDType> + </Compartment> + <Compartment Desc="Definition des Compartments" ID="3"> + <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">bulk</CompartmentType> + <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes> + <ULDType Desc="Definition der Containergruppe" ID="1"> + <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD> + <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow> + <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">1</ULDs> + </ULDType> + </Compartment> + </CargoDeck> + </Cargo> + <Propulsion Desc="Vorgaben zum Antriebssystem"> + <TypeOfEngine Desc="Triebwerkstechnologie (Jet oder Prop)" Unit="-">Jet</TypeOfEngine> + <NumberOfEngines Desc="Anzahl der Triebwerke">2</NumberOfEngines> + <PositionOfEngines Desc="Positionierung der Triebwerke"> + <EnginesOnWing Desc="Anzahl der Triebwerke am Fluegel">2</EnginesOnWing> + <EnginesOnFuselage Desc="Anzahl der Triebwerke am Rumpf, mit Pylons montiert">0</EnginesOnFuselage> + <EnginesInFuselage Desc="Anzahl der Triebwerke im Rumpf integriert">0</EnginesInFuselage> + <WingEnginePosition Desc="0=EngineUnderWing; 1= EnginesOverWing">0</WingEnginePosition> + </PositionOfEngines> + <FuelDensity Desc="Dichte des Kraftstoffs" Unit="kg/l">0.785</FuelDensity> + </Propulsion> + <TankConfiguration Desc="Vorgaben zur Aufteilung der Tanks"> + <NumberOfCenterTanks Desc="Anzahl der Tanks im Rumpf (Fluegelkasten + zus. Tanks)">1</NumberOfCenterTanks> + <NumberOfWingTanks Desc="Anzahl der Tanks im Fluegel">2</NumberOfWingTanks> + <NumberOfTrimTanks Desc="Anzahl der Tanks zur Trimmung">0</NumberOfTrimTanks> + </TankConfiguration> + <HighLiftSystem Desc="Vorgaben zum Hochauftriebssystem"> + <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert in Startkonfiguration. Statistik, falls Wert 0" Unit="-">2.3</C_LmaxT-O> + <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert in Landekonfiguration. Statistik, falls Wert 0" Unit="-">2.8</C_LmaxLanding> + </HighLiftSystem> + <DesignLoads Desc="Vorgaben zu zulaessigen Lastvielfachen"> + <n1 Desc="maximum positive load limit (CS-25: n1=2.5g)" Unit="g">2.5</n1> + <n2 Desc="maximum negative load limit (CS-25: n2=-1.0g)" Unit="g">-1</n2> + </DesignLoads> + <Technology Desc="Vorgaben spezieller Technologien"> + <LaminarFlow Desc="HLFC oder NLF"> + <Components Desc="Flugzeugkomponenten, auf die HLFC/NLF angewendet wird"> + <Wing> + <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide> + <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide> + </Wing> + <Stabilizer> + <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide> + <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide> + </Stabilizer> + <Fin Desc="Seitenleitwerk (HLFC, NLF, None)">None</Fin> + <Nacelles Desc="Triebwerksgondeln (HLFC, NLF, None)">None</Nacelles> + </Components> + </LaminarFlow> + <ElectricTaxiing> + <DoElectricTaxiing Desc="1: Electric Taxiing, 0: Propulsion Taxiing">0</DoElectricTaxiing> + <EngineWarmupTime Desc="Laufzeit der Triebwerke vor dem Start" Unit="min">0</EngineWarmupTime> + </ElectricTaxiing> + <BallisticRecoverySystem Desc="Ballistic Recovery System (Parachute)">0</BallisticRecoverySystem> + </Technology> + </DesignSpecification> +</AcftExchangeFile>