[fltsim.0] title=Tupolev Tu-144 sim=Tu-144 model= panel= sound= texture= checklists= ui_manufacturer=Tupolev ui_type=Tu 144 ui_variation=Aeroflot description=The Tu-144 was the world's first supersonic airliner to take flight, beating the Concorde into the air by three months. atc_heavy=0 atc_id= atc_airline=Aeroflot atc_flight_number= [General] atc_type= atc_model= [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) empty_weight_roll_MOI=30500118.00 empty_weight_pitch_MOI=32500118.00 empty_weight_yaw_MOI=8506663.00 empty_weight_coupled_MOI=20000.00 max_gross_weight= 409107.994 [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=1.500 [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=1.300 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 [fuel] Center1=-11.00,0.00,0.00,7875.00,0.00 Center2=-99.00,0.00,0.00,3645.00,0.00 LeftMain=-55.00,-14.600000,-4.500000,10000.00,0.00 RightMain=-55.00,14.600000,-4.500000,10000.00,0.00 fuel_type=2.00 number_of_tank_selectors=1 [airplane_geometry] wing_area=4310.00 wing_span=84.00 wing_root_chord=66.166667 wing_dihedral=3.999023 wing_incidence=0.247192 wing_twist=1.999512 oswald_efficiency_factor=0.697116 wing_winglets_flag=0 wing_sweep=0.00 wing_pos_apex_lon=0.00 wing_pos_apex_vert=0.00 htail_area=0.00 htail_span=0.00 htail_pos_lon=0.00 htail_pos_vert=0.00 htail_incidence=0.00 htail_sweep=0.00 vtail_area=249.00 vtail_span=17.991665 vtail_sweep=0.00 vtail_pos_lon=-125.00 vtail_pos_vert=23.333333 elevator_area=70.500000 aileron_area=26.800000 rudder_area=56.200000 elevator_up_limit=29.793805 elevator_down_limit=29.793805 aileron_up_limit=29.793805 aileron_down_limit=29.793805 rudder_limit=30.000070 elevator_trim_limit=19.996227 spoiler_limit=0.00 spoilerons_available=1 aileron_to_spoileron_gain=3.00 min_ailerons_for_spoilerons=9.969466 min_flaps_for_spoilerons=0.00 [contact_points] point.0=1.00, 8.7,0.00,-16.950000,1241.176335,0.00,3.336104,34.080000,1.000000,2.000000,0.980000,5.00,5.00,0.00,0.00,0.00 point.1=1.00,-54.00,-13.00,-13.47,1574.803150,1.00,3.336104,0.00,1.500000,2.500000,1.00,7.900000,7.900000,2.00,0.00,0.00 point.2=1.00,-54.00,13.00,-13.47,1574.803150,2.00,3.336104,0.00,1.500000,2.500000,1.00,8.100000,8.100000,3.00,0.00,0.00 point.3=2.00,-14.166667,-47.333333,0.00,1388.141302,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00 point.4=2.00,-14.166667,47.333333,0.00,1388.141302,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00 point.5=2.00,-116.666667,0.00,-0.833333,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00 point.6=2.00,47.666667,0.00,-6.666667,787.401575,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00 point.7=2.00,47.666667,0.00,5.916667,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,7.00,0.00,0.00 point.8=2.00,-125.00,23.333333,0.00,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,8.00,0.00,0.00 static_pitch=4.65 static_cg_height=14.25 [Flaps.0] type=1 span-outboard=0.500000 extending-time=10.00 system_type=0 flaps-position.0=0.00,0.00 flaps-position.1=2.864789,0.00 flaps-position.2=5.729578,0.00 [GeneralEngineData] engine_type=1 Engine.0=-38.00,-19.250000,-1.00 Engine.1=-38.00,-15.250000,-1.00 Engine.2=-38.00,15.250000,-1.00 Engine.3=-38.00,19.250000,-1.00 fuel_flow_scalar=1.00 [TurbineEngineData] fuel_flow_gain=0.002000 inlet_area=16.00 rated_N2_rpm=18288.00 static_thrust=31000.00 afterburner_available=1 reverser_available=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -54.14, -45.24, -4.2, fx_navredm , light.1=3, -54.14, 45.24, -4.2, fx_navgrem , light.2=3, -90.32, 0.00, 29.52, fx_navwhih , light.3=2, -53.22, -45.08, -4.2, fx_strobeh , light.4=2, -53.22, 45.08, -4.2, fx_strobeh , light.5=2, 22.65, 0.00, -4.00, fx_beaconb , light.6=1, 6.20, 0.00, 8.30, fx_beaconh , light.7=4, 44.41, 0.00, 3.50, fx_vclight , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [Reference Speeds] flaps_up_stall_speed=142.00 full_flaps_stall_speed=113.600000 cruise_speed=1152.924110 [keyboard_response] elevator=150.00,250.00 aileron=150.00,250.00 rudder=150.00,250.00 [Views] eyepoint=41.664104,-1.307210,4.267655 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.00 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.00 pitch_takeoff_ga=8.00 [direction_indicators] direction_indicator.0=3,0
