; Modified for use with customized AIR file. Both files MUST be used ; together for proper performance. ; Paul R. Varn pvarn@speakeasy.org ; Modified for FS2002 10/17/2002 ; Updated 01/20/2002 ; Editing with FSEdit will destroy this model or cause ; FSEdit to lock up [fltsim.0] title=Concorde G sim=Concorde model= panel= sound= texture= kb_checklists=Concorde_check kb_reference=Concorde_ref atc_id=N700MS atc_airline=Britsh Airways atc_type=CONCORDE atc_flight_number=PV01 ui_manufacturer=British Aerospace ui_type=Concorde ui_variation=British Airways description=This is your opportunity to fly the world's only supersonic \nairliner. After nearly three decades of airline service, \nConcorde is still an exciting and exotic airplane. \nTake off from London at midnight and arrive in \nNew York three and a half hours later-on the day before \nyou took off. Modified for FS2002 by Paul R. Varn 01/20/2001 atc_heavy=1 [WEIGHT_AND_BALANCE] empty_weight=172671.000 reference_datum_position=0.000, 0.000, 0.000 // Center of weight for the whole aircraft: empty_weight_CG_position=-50.333, 0.000, 0.000 // Controls CG pumping in concorde (orig=-36.519) station_load.0=1686.000, 1.000, 0.000, 0.000 station_load.1=3342.000, -29.000, 0.000, 0.000 station_load.2=300.000, 8.000, 0.000, 0.000 station_load.3=500.000, -4.000, 0.000, 0.000 station_load.4=2562.000, -82.000, 0.000, 0.000 station_load.5=2966.000, 18.000, 0.000, 0.000 station_load.6=2966.000, 2.000, 0.000, 0.000 station_load.7=4296.000, -28.000, 0.000, 0.000 station_load.8=6006.000, -53.000, 0.000, 0.000 empty_weight_roll_MOI=2000118.000 empty_weight_pitch_MOI=26500118.000 empty_weight_yaw_MOI=7506663.000 empty_weight_coupled_MOI=0.000 max_gross_weight=407154.000 CG_forward_limit=0.100 CG_aft_limit=0.800 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) fuel_transfer_pump=0, 10, 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=1.600 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=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [fuel] Center1=-10.000, 0.000, 0.000, 7695.000, 0.000 Center2=-110.000, 0.000, 0.000, 3479.000, 0.000 LeftMain=-54.671, -14.600, -4.500, 10173.000, 0.000 RightMain=-54.671, 14.600, -4.500, 10173.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=4262.000 wing_span=83.833 wing_root_chord=66.167 wing_dihedral=0.000 wing_incidence=0.247 wing_twist=0.000 oswald_efficiency_factor=0.904 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=0.100 htail_span=0.100 htail_pos_lon=0.000 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=249.000 vtail_span=17.992 vtail_sweep=0.000 vtail_pos_lon=-35.833 vtail_pos_vert=5.833 elevator_area=70.500 aileron_area=26.800 rudder_area=56.200 elevator_up_limit=29.794 elevator_down_limit=29.794 aileron_up_limit=29.794 aileron_down_limit=29.794 rudder_limit=30.000 elevator_trim_limit=19.996 spoiler_limit=0.000 spoilerons_available=1 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=9.969 min_flaps_for_spoilerons=0.000 [contact_points] point.0=1.000, 5.667, 0.000, -14.000, 1181.102, 0.000, 3.336, 34.080, 1.500, 2.500, 0.950, 5.000, 5.000, 0.000, 0.000, 0.000 point.1=1.000, -54.000, -13.000, -14.000, 1574.803, 1.000, 3.336, 0.000, 1.500, 2.500, 0.950, 7.900, 7.900, 2.000, 0.000, 0.000 point.2=1.000, -54.000, 13.000, -14.000, 1574.803, 2.000, 3.336, 0.000, 1.500, 2.500, 0.950, 8.100, 8.100, 3.000, 0.000, 0.000 point.3=2.000, -14.167, -47.333, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.000, -14.167, 47.333, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.000, -116.667, 0.000, 0.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, 42.667, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.280 static_cg_height=12.720 [GeneralEngineData] engine_type=1 Engine.0=-38.000, -19.250, -1.000 Engine.1=-38.000, -15.250, -1.000 Engine.2=-38.000, 15.250, -1.000 Engine.3=-38.000, 19.250, -1.000 fuel_flow_scalar=1.000 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=12.500 rated_N2_rpm=18288.000 static_thrust=30400.000 afterburner_available=1 reverser_available=1 [Reference Speeds] //knots (true) flaps_up_stall_speed=150.000 full_flaps_stall_speed=150.000 cruise_speed=1130.000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=56.671383,-1.281578,9.188915 [General] performance=Length: 202 ft\nSpan: 83.3 ft\nWing Area: 3,926 ft^2\nHeight: 40ft\nMax Speed\tM 2.22\nCruise Speed\tMach 2.1\nMaximum Range\t4,100 nm \nFuel Rate 55K ft cruise: 31.5K lbs\/hr, 3.6 kg\/hr\/eng\nService Ceiling: 60,000 ft\nMax Takeoff Weight: 408,000 lb\nSeating: 128\nMax Payload: 29,000 lb\nMax Landing Weight: 244,486lbs \n(80,207 lbs fuel - 36,532 kg)\nMin Take Off Roll: 6,562ft\nMin Land Roll: 6,562ft\nModified by Paul Varn 10\/22\/2001\nMUST be used with matching aircraft.cfg file\n atc_type= atc_model= [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=108.500000 pitch_takeoff_ga=13.500000 use_no_default_pitch=1 use_no_default_bank=1 ;[pitot_static] vertical_speed_time_constant=12 ;[direction_indicators] direction_indicator.0=3,0 [Radios] Audio.1=1 Com.1=1,1 Com.2=1,1 Nav.1=1,0,1 Nav.2=1,0,0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=1, 0.00, 0.00, 0.01, fx_vclighth , light.1=4, 0.53, -1.30, 0.00, fx_vcfloodltm , light.2=4, 0.53, 1.30, 0.00, fx_vcfloodltm , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [SMOKESYSTEM] smoke.0=-5.00, -75.00, 18.00, fx_smoke_rx smoke.1=-5.00, -75.00, 15.00, fx_smoke_rx smoke.2=-5.00, -75.00, -15.00, fx_smoke_rx smoke.3=-5.00, -75.00, -18.00, fx_smoke_rx [Flaps.0] type=1 span-outboard=0.125 extending-time=8.000 system_type=0 damaging-speed=325.000 blowout-speed=330.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=2.000, 0.000 flaps-position.1=5.000, 0.000 flaps-position.2=8.000, 0.000 [direction_indicators] direction_indicator.0=3,0