[fltsim.0]
title=Tu-160
sim=Tu-160
model=
panel=
sound=
texture=
sound_alias=B737_400\sound
kb_checklists=
kb_reference=
atc_id=N700MS
atc_airline=
atc_flight_number=0001
atc_heavy=1
ui_manufacturer=Tupolev Design Bureau
ui_type=Tu-160 Blackjack
ui_variation=Paint1
description=The Tu-160 is a multi-mission strategic bomber designed for operations ranging from subsonic speeds and low altitudes to speeds over Mach 1 at high altitudes. The two weapons bays can accommodate different mission-specific loads, including strategic cruise missiles, short-range guided missiles, nuclear and conventional bombs, and mines. Its basic armament of short-range guided missiles and strategic cruise missiles enables it to deliver nuclear strikes to targets with preassigned coordinates.In the future, after the aircraft is equipped with high-precision conventional weapons it may also be used against mobile or tactical targets.
[fltsim.1]
title=Tu-160 Pant2
sim=Tu-160
model=
panel=
sound=
texture=1
sound_alias=B737_400\sound
kb_checklists=
kb_reference=
atc_id=N700MS
atc_airline=
atc_flight_number=0001
atc_heavy=1
ui_manufacturer=Tupolev Design Bureau
ui_type=Tu-160 Blackjack
ui_variation=Paint2
description=Tu-160
[General]
atc_type=
atc_model=
performance=Soviet Designation\n TU-160\n \nUS-Designation\n Blackjack\n \nDesign Bureau\n OKB-156 Tupolev\n \nManufacturer\n Plant Nr. 22 Kazan\n \nPower Plant\n 4 HK-32 turbojet engines\n \nThrust\n 25.000 kg each\n \nLength\n 54.1\n \nHeight\n 13.1\n \nWingspan\n 35.6m (minimum), 55.7m (maximum)\n \nWing surface\n 232 sqm\n \nSpeed\n 2200 km\/h (maximum), 1030 km\/h (ground)\n \nCeiling\n 16.000m\n \nWeight (empty)\n 110.000kg \n \nFuel weight\n 148.000 kg\n \nMaximum take-off weight\n 275.000 kg\n \nNormal load\n 9.000 kg\n \nMaximum load\n 40.000\n \nRange\n 14.000 km (with a load of 9.000kg)\n\n10.500 km (with a load of 40.000 kg)\n \nArmament\n 12 H-55 or 24 H-15 missiles\n\nfree falling bombs\n \nSystems\n \nCrew\n 4\n \nAccomodation\n \nUnit cost\n \nApproved\n \nDevelopment began\n 1975\n \nFirst Flight\n 12\/19\/1981\n \nSeries production started \n 1984\n \nDate deployed\n 1987\n \n
[pitot_static]
vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight= 606260.000
empty_weight=242504.000
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=-17.000, 0.000, 0.000
max_number_of_stations=50
;Moments of Inertia
empty_weight_roll_MOI=2262183.000
empty_weight_pitch_MOI=3172439.000
empty_weight_yaw_MOI=3337024.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000
station_load.0=88183.000, -17.000, 0.000, 0.000
[fuel]
Center1=-15.000, 0.000, 0.000, 5500.000, 3.000
Center2=-17.000, 0.000, 0.000, 5500.000, 3.000
LeftMain=-17.000, -19.000, 0.000, 5000.000, 3.000
LeftAux=-15.000, 0.000, 0.000, 500.000, 3.000
RightMain=-17.000, 19.000, 0.000, 5000.000, 3.000
RightAux=-17.000, 0.000, 0.000, 500.000, 3.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[airplane_geometry]
wing_area=2137.000
wing_span=116.000
wing_root_chord=18.000
wing_dihedral=2.200
wing_incidence=0.000
wing_twist=-0.500
oswald_efficiency_factor=0.820
wing_winglets_flag=0
wing_sweep=45.000
wing_pos_apex_lon=17.000
wing_pos_apex_vert=2.000
htail_area=690.000
htail_span=41.700
htail_pos_lon=-72.000
htail_pos_vert=16.000
htail_incidence=0.000
htail_sweep=30.000
vtail_area=691.000
vtail_span=22.000
vtail_sweep=35.000
vtail_pos_lon=-75.000
vtail_pos_vert=16.000
elevator_area=70.500
aileron_area=26.900
rudder_area=56.200
elevator_up_limit=21.000
elevator_down_limit=10.000
aileron_up_limit=20.000
aileron_down_limit=20.000
rudder_limit=26.000
elevator_trim_limit=10.000
spoiler_limit=60.000
spoilerons_available=1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=0.000
[Reference Speeds]
flaps_up_stall_speed= 150.000
full_flaps_stall_speed= 120.000
cruise_speed= 900.000
[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
[GeneralEngineData]
engine_type=1
Engine.0=-26.750, -11.480, 0.000
Engine.1=-26.750, 11.480, 0.000
Engine.2=-26.760, -17.500, 0.000
Engine.3=-26.760, 17.500, 0.000
fuel_flow_scalar=1.000
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=30.600
rated_N2_rpm=29920.000
static_thrust=40892.500
afterburner_available=1
reverser_available=1
[jet_engine]
thrust_scalar=1.000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
[contact_points]
//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)
point.0= 1.000, 40.650, 0.000, -7.800, 2500.000, 0.000, 2.000, 70.000, 0.500, 6.500, 0.900, 9.000, 8.000, 0.000, 0.000, 0.000
point.1= 1.000, -17.900, -12.580, -9.580, 4000.000, 1.000, 2.400, 13.000, 3.000, 2.500, 0.900, 11.000, 9.000, 2.000, 0.000, 0.000
point.2= 1.000, -17.900, 12.580, -9.580, 4000.000, 2.000, 2.400, 13.000, 3.000, 2.500, 0.900, 11.000, 9.000, 3.000, 0.000, 0.000
point.3= 2.000, -14.700, -47.330, 0.000, 700.000, 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, -14.700, -47.330, 0.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
static_pitch= 0.640
static_cg_height= 7.660
[Views]
eyepoint=-19.4, -1.97, 9.27 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 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
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.7=1, -77, 0.00, 32,fx_beacon,
[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
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[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= 1.000
extending-time= 15.000
system_type= 0
damaging-speed= 800.000
blowout-speed= 1000.000
lift_scalar= 0.050
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
