[fltsim.0] title=Concorde Virgin Atlantic sim=Concorde model= panel= sound= texture= kb_checklists=Concorde_check kb_reference=Concorde_ref atc_type=Concorde atc_id_enable=1 atc_id=G-CONC [WEIGHT_AND_BALANCE] empty_weight=172930.0 // (pounds) reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-50.333, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum station_load.0=1760, 1.00, 0.0, 0.0 //Weight Crew (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=3342, -29.00, 0.0, 0.0 //Weight Galleys(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=300, 8.00, 0.0, 0.0 //Weight Baggage 1 (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=500, -4.00, 0.0, 0.0 //Weight Baggage 2 (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=2562, -82.00, 0.0, 0.0 //Weight Baggage 3 (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=3040, 18.00, 0.0, 0.0 //Weight Psgr Sect OA (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=3040, 2.00, 0.0, 0.0 //Weight Psgr Sect OB (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7=4370, -28.00, 0.0, 0.0 //Weight Psgr Sect OC (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8=6080, -53.00, 0.0, 0.0 //Weight Psgr Sect OD (lbs), longitudinal, lateral, vertical positions from datum (feet) [ground_reaction] main_gear_static_compression=1.5 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=1.5 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=1.00 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=0.98 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage=24 ;Voltage of the battery when fully charged. In Volts. generator_alternator_voltage=30 ;The voltage produced by the alternator/generator, in Volts. max_generator_alternator_amps=70 fuel_transfer_pump=0, 10, 17.0 flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=3, 6 , 17.0 starter1=3, 20, 17.0 starter2=3, 20, 17.0 starter3=3, 20, 17.0 starter4=3, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [jet_engine] thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=1.870 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=0.6 rudder_trim_effectiveness=0.6