[fltsim.0] title=Tupolev Tu-360 sim=tu360 model= panel= sound= texture= panel_alias= sound_alias= kb_checklists= kb_reference= atc_id=02 atc_airline=AIRFORCE atc_flight_number= ui_manufacturer=Tupolev ui_type=Tu-360 ui_variation=White description=The Tu-360 hypersonic bomber was designed in the 1980s by a team led by V. A. Andreyev at the Tupolev OKB. It was to carry a 10,000 kg offensive load to a distance of 15,000 km at a speed of Mach 6. Power was to be supplied by six variable-cycle turboramjet engines fuelled with liquid hydrogen. Armament was carried in two weapon bays located in the wingroots, crew consisting of two pilots. According to the draft design, the range requirement could not be achieved, maximum range at Mach 6 being 9,000-10,000 km. atc_heavy=1 [General] atc_type= atc_model= performance=Cruise Speed \nMach 6\n\nEngines \nSix liquid hydrogen fuelled turboramjets\n\nMaximum Range \n10,000 km 5,400 nm\n\nService Ceiling \n30,000 m 98,430 ft\n\nMaximum Takeoff Weight \n350,000 kg 771,400 lb\n\nEmpty Weight\n200,000 kg 440,800 lb\n\nLength \n100 m 328 ft\n\nWingspan \n40.7 m 133.53 ft\n\nWing Area\n1,250 m2 13,455 sq ft\n\nPayload \n10,000 kg 22,040 lb\nof armament in two weapon bays\n [WEIGHT_AND_BALANCE] max_gross_weight=771400.000 empty_weight=440800.000 reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI=100000000.000 empty_weight_roll_MOI=18000000.000 empty_weight_yaw_MOI=51000000.000 empty_weight_coupled_MOI=1200.000 CG_forward_limit=0.000 CG_aft_limit=1.000 max_number_of_stations=50 station_load.0=1.000000, -28.000000, 18.800000, 1.000000 station_load.1=1.000000, -28.000000, -18.800000, 1.000000 [flight_tuning] cruise_lift_scalar=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=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [jet_engine] thrust_scalar=1.000 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot=0,5,17.000 avionics_bus=0,10,17.000 avionics=1,5,17.000 pitot_heat=0,2,17.000 marker_beacon=1,2,17.000 gear_warning=0,2,17.000 fuel_pump=0,5,17.000 light_nav=0,5,17.000 light_beacon=0,5,17.000 light_taxi=0,5,17.000 light_strobe=0,5,17.000 light_panel=0,5,17.000 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0=1.000, 81.200, 0.000, -24.700, 1181.100, 0.000, 2.200, 34.100, 1.000, 2.500, 0.800, 6.000, 6.000, 0.000, 0.000, 0.000 point.1=1.000, -36.300, -29.500, -21.500, 1574.800, 1.000, 2.500, 0.000, 1.000, 2.500, 0.800, 7.900, 7.900, 2.000, 0.000, 0.000 point.2=1.000, -36.300, 29.500, -21.500, 1574.800, 2.000, 2.500, 0.000, 1.000, 2.500, 0.800, 7.900, 7.900, 3.000, 0.000, 0.000 point.3=2.000, -61.000, -66.750, 0.000, 787.400, 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, -61.000, 66.750, 0.000, 787.400, 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, -91.600, 0.000, -4.300, 1574.800, 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, 176.000, 0.000, -4.300, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=1.000 static_cg_height=23.000 [Views] eyepoint=152.8, -2.7, 9.9 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=0 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150, 250 aileron=150, 250 rudder=150, 250 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [LIGHTS] //lon, lat, vert //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1=2, -22.0, 0.0, 20.9, fx_beacon light.2=2, 8.0, 0.0, -3.9, fx_strobe light.3=3, -65.0, 65.3, 0.2, fx_navgre light.4=3, -65.0, -65.3, 0.2, fx_navred [fuel] Center1=46.000, 0.000, 11.000, 10000.000, 0.000 Center2=-36.000, 0.000, 11.000, 10000.000, 0.000 LeftMain=-52.000, -45.000, 0.000, 7440.000, 0.000 RightMain=-52.000, 45.000, 0.000, 7440.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 [airplane_geometry] wing_area=13455.000 wing_span=133.500 wing_root_chord=83.000 wing_dihedral=0.000 wing_incidence=2.000 wing_twist=0.000 oswald_efficiency_factor=20.000 wing_winglets_flag=0 wing_sweep=65.000 wing_pos_apex_lon=65.200 wing_pos_apex_vert=0.000 htail_area=210.000 htail_span=50.000 htail_pos_lon=-75.000 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=35.000 vtail_area=249.000 vtail_span=50.500 vtail_sweep=60.000 vtail_pos_lon=-142.000 vtail_pos_vert=73.000 elevator_area=136.000 aileron_area=124.000 rudder_area=56.200 elevator_up_limit=30.000 elevator_down_limit=20.000 aileron_up_limit=20.000 aileron_down_limit=15.000 rudder_limit=25.000 elevator_trim_limit=20.000 spoiler_limit=0.000 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [GeneralEngineData] engine_type=1 Engine.0=-58.000, -9.400, -6.500 Engine.1=-58.000, -4.700, -6.500 Engine.2=-58.000, 4.700, -6.500 Engine.3=-58.000, 9.400, -6.500 fuel_flow_scalar=1.000 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=72.000 //doubled rated_N2_rpm=29920.000 static_thrust=130000.000 afterburner_available=1 reverser_available=0 [Reference Speeds] flaps_up_stall_speed=143.000 full_flaps_stall_speed=120.000 cruise_speed=2400.000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8 [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 [Flaps.0] type=1 span-outboard=0.200 extending-time=5.000 system_type=0 damaging-speed=500.000 blowout-speed=800.000 lift_scalar=0.500 drag_scalar=1.100 pitch_scalar=1.300 flaps-position.0=0.000, 0.000 flaps-position.1=10.000, 0.000 flaps-position.2=20.000, 0.000 flaps-position.3=30.000, 0.000 [Flaps.1] type=1 span-outboard=0.200 extending-time=5.000 system_type=0 damaging-speed=500.000 blowout-speed=800.000 lift_scalar=0.500 drag_scalar=1.100 pitch_scalar=1.300 flaps-position.0=0.000, 0.000 flaps-position.1=0.000, 0.000 flaps-position.2=10.000, 0.000 flaps-position.3=20.000, 0.000
