[fltsim.0]
title=Tupolev Tu-128
sim=Tu-128
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=45032
atc_airline=Air Force
atc_flight_number=8
ui_manufacturer=Tupolev
ui_type=Tu-128 Fiddler
ui_variation="Russia VVS"
description=Model by Vitaly Nikolaev
atc_id_color=0x00000000
visual_damage=0
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0

[General]
atc_type=TUPOLEV 
atc_model=Tu-124 
editable=0 
performance="Maximum range: 1595 nm\nMaximum range ceiling: 51184 ft\nCruise speed : M 1.1\nCrew: 2\nMTOW: 96342 lbs\nTakeoff distance: 7550 ft" 
Category=airplane

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[weight_and_balance]

// ACM V2.5
max_gross_weight = 96342
empty_weight = 54013 
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 752312
empty_weight_roll_MOI = 227631
empty_weight_yaw_MOI = 666771
empty_weight_coupled_MOI = 0
max_number_of_stations = 3

station_load.0 = 530.0,  36.7,  0.0,	0.0,
station_load.1 = 9270, 2.53, 0, 0
station_load.2 = 3973, 1.62, 0, 0


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -22.51, -28.51, -2.02, fx_navredm.fx
light.3 = 3, -22.54, 28.61, -2.02, fx_navgrem.fx
light.4 = 3, -36.85, 0, 1.77, fx_navwhih.fx
light.5 = 2, 17.57, 0, -3.40, fx_beaconh.fx
light.6 = 4, 39.32, 0, 2.43, fx_vclight_yellow.fx
light.7 = 4, 34.45, 0, 2.99, fx_vclight_yellow.fx
light.8 = 9, -36.88, 2, 0, fx_flankerflame.fx
light.9 = 9, -36.88, -2, 0, fx_flankerflame.fx
light.10 = 9, -36.88, 2, 0, fx_flankerburner.fx
light.11 = 9, -36.88, -2, 0, fx_flankerburner.fx
light.12= 10, -10.0,  0.0,  0.0,   fx_RCB_machenvlop.fx   // SonicBoom effect

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.826
min_throttle_limit = -0.250000
engine.0 = 4.75, -7.33, -1.0
engine.1 = 4.75,  7.33, -1.0

[smokesystem]


[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

Center1 = 1.26, 0, 0, 1151.7, 0
LeftAux = -8, -26.5, 0, 393.27, 0
LeftTip = -15, -34.5, 0, 125, 0
RightAux = -8, 26.5, 0, 393.27, 0
RightTip = -15, 34.5, 0, 125, 0
LeftMain = 0, -11.6, 0, 1049.66, 0
RightMain = 0, 11.6, 0, 1049.66, 0


[contact_points]
static_pitch = 3
static_cg_height = 9.0
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 8

point.0 = 1, 29.5341, 0, -9.786, 910, 0, 1.082, 35, 0.37, 2.8, 0.78, 10.9, 10.9, 0, 237.5, 260
point.1 = 1, -3.255, -10.2993, -8.4405, 1075, 1, 1.418, 0, 0.393, 1.17, 0.79, 12, 11.8, 2, 237.5, 260
point.2 = 1, -3.2548, 10.2988, -8.4636, 1075, 2, 1.418, 0, 0.393, 1.17, 0.79, 12, 11.9, 3, 237.5, 260
point.3 = 2, -15.2798, -28.4221, -2.2256, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -15.2798, 28.4112, -2.1572, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -36.0804, 0, -1.7978, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 56.1549, 0, -1.5725, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 5, -30.8157, 0, -2.4092, 1600, 0, 0, 50, 0, 0, 1, 2, 2, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
//ACM_AREAW1// 0,0,0,5.9253,1.4191,1.4191,0.9937,6.6227,2.8387,2.8387
//ACM_AREAW2// 1.9874,7.3204,4.2579,4.2579,2.9814,8.0179,5.6774,5.6774,3.9753,8.7156
//ACM_AREAW3// 7.0967,7.0967,4.9692,9.4131,8.5158,8.5158,5.9629,10.1106,9.9354,9.9354
//ACM_AREAW4// 6.9566,10.8083,11.3548,11.3548,7.9506,11.5059,12.7741,12.7741,8.9441,12.2033
//ACM_AREAH1// 0,0,0,3.3231,0.5536,0.5536,0.4986,3.6558,1.1073,1.1073
//ACM_AREAH2// 0.9973,3.9883,1.6612,1.6612,1.4960,4.3210,2.2155,2.2155,1.9946,4.6535
//ACM_AREAH3// 2.7692,2.7692,2.4934,4.9861,3.3231,3.3231,2.9923,5.3186,3.8770,3.8770
//ACM_AREAH4// 3.4909,5.6511,4.4310,4.4310,3.9897,5.9836,4.9850,4.9850,4.4885,6.3161
//ACM_AREAV1// 0,0,0,4.1146,0.4571,0.4571,0.4115,4.1971,0.9143,0.9143
//ACM_AREAV2// 0.8233,4.2796,1.3716,1.3716,1.2345,4.3621,1.8286,1.8286,1.6466,4.4446
//ACM_AREAV3// 2.2860,2.2860,2.0583,4.5272,2.7432,2.7432,2.4697,4.6096,3.2002,3.2002
//ACM_AREAV4// 2.8815,4.6921,3.6575,3.6575,3.2932,4.7746,4.1146,4.1146,3.7049,4.8571
//ACM_CAREAW1// 6.3870,6.3870,7.4348,8.6197,7.0967,7.0967,7.9317,9.0576,7.8063,7.8063
//ACM_CAREAW2// 8.4287,9.4953,8.5158,8.5158,8.9257,9.9329,9.2257,9.2257,9.4224,10.3704
//ACM_CAREAW3// 9.9354,9.9354,9.9195,10.8083,10.6450,10.6450,10.4160,11.2460,11.3548,11.3548
//ACM_CAREAW4// 10.9132,11.6836,12.0642,12.0642,11.4103,12.1211,12.7741,12.7741,11.9069,12.5590
//ACM_CAREAH1// 0,0,1.6612,3.3231,0.5536,0.5536,2.1603,3.7388,1.1073,1.1073
//ACM_CAREAH2// 2.6591,4.1546,1.6612,1.6612,3.1577,4.5700,2.2155,2.2155,3.6565,4.9857
//ACM_CAREAH3// 2.7692,2.7692,4.1552,5.4015,3.3231,3.3231,4.6539,5.8171,3.8770,3.8770
//ACM_CAREAH4// 5.1525,6.2328,4.4310,4.4310,5.6514,6.6483,4.9850,4.9850,6.1501,7.0640
//ACM_CAREAV1// 0,0,1.0283,3.0861,0.4571,0.4571,1.4400,3.3331,0.9143,0.9143
//ACM_CAREAV2// 1.8516,3.5801,1.3716,1.3716,2.2636,3.8273,1.8286,1.8286,2.6751,4.0742
//ACM_CAREAV3// 2.2860,2.2860,3.0868,4.3214,2.7432,2.7432,3.4986,4.5685,3.2002,3.2002
//ACM_CAREAV4// 3.9103,4.8154,3.6575,3.6575,4.3220,5.0626,4.1146,4.1146,4.7336,5.3097
wing_area = 1043.46
wing_span = 57.51
wing_root_chord = 19.44
wing_dihedral = -1.0
wing_incidence = 1.0
wing_twist = -1.5
oswald_efficiency_factor = 0.89
wing_winglets_flag = 0
wing_sweep = 35.0
wing_pos_apex_lon = 17.8
wing_pos_apex_vert = 0.0
htail_area = 285.79
htail_span = 32.71
htail_pos_lon = -36.70
htail_pos_vert = 3.70
htail_incidence = -1.0
htail_sweep = 42.0
vtail_area = 131.32
vtail_span = 13.5
vtail_sweep = 42.51
vtail_pos_lon = -39.0
vtail_pos_vert = 8.1
elevator_area = 71.69
aileron_area = 65.23
rudder_area = 61.61
elevator_up_limit = 29.0
elevator_down_limit = 19.9
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 26.0
elevator_trim_limit = 20.0
spoiler_limit = 52.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=1.0 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
pitch_stability=1.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=0.821 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 

[TurbineEngineData]
fuel_flow_gain=0.0010                          //Gain on fuel flow
inlet_area=8.9462                               //Square Feet, engine nacelle inlet area
rated_N2_rpm=11700.00                           //RPM, second stage compressor rated value
static_thrust= 22270                          //Lbs, max rated static thrust at Sea Level ----16370
afterburner_available=6                       //Afterburner available?
afterburner_throttle_threshold = 0.80           //Percent of throttle range where a/b begins
reverser_available=0                          //Thrust reverser available?
bypass_ratio=1.00

[jet_engine]
thrust_scalar=1.0 

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1         //Parking brake available
toe_brakes_scale = 0.885  //Brake scalar
auto_brakes=4

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint=36.96, -0.51, 2.43   //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.61                                  // 0.0 .. 1.0
extending-time   = 21                                   // seconds
flaps-position.0 = 0.0                                    // degrees
flaps-position.1 = 10                                    // degrees
flaps-position.2 = 15                                    // degrees
flaps-position.3 = 30                                    // degrees
damaging-speed   = 216                                  // KIAS
blowout-speed    = 244                                  // KIAS
lift_scalar = 1.32
drag_scalar = 0.65
pitch_scalar= 0.95
system_type = 0                                         //Electromechanic

[flaps.1]       //tormoznoy shchitok
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 4.28                                  // 0.0 .. 1.0
extending-time   = 3                                    // seconds
flaps-position.0 = 0.0                                    // 
flaps-position.1 = 0.0                                    // degrees
flaps-position.2 = 0.0                                    // degrees
flaps-position.3 = 0.0                                  // 
flaps-position.4 = 40.0                                  // 
damaging-speed   = 167                                  // KIAS
blowout-speed    = 216                                  // KIAS
lift_scalar = 0.00
drag_scalar = 1.05
pitch_scalar= 0.0
system_type = 0                                         //Electromechanic

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1, 0 
Com.2=1, 0 
Nav.1=1, 0, 1 
Nav.2=1, 0, 0 
Adf.1=1 
Adf.2=1 
Transponder.1=1 
Marker.1=1 

[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 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0= 1

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800 
autothrottle_available=1 
autothrottle_arming_required=0
autothrottle_max_rpm = 120
autothrottle_takeoff_ga=1
pitch_takeoff_ga=7 ;
max_pitch=12.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0


[stall_warning]
type=2
re feet
wing_span               = 83.82                 //Feet
wing_root_chord         = 19.44                  //Feet
wing_dihedral           = -1.0                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -2.0                  //Degrees
oswald_efficiency_factor= 0.89                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 35.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = 6.6                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 285.79                 //Square feet
htail_span              = 32.71                  //Feet
htail_pos_lon           = -40.36                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 5.19                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = -1.0                   //Degrees
htail_sweep             = 42.0                  //Degrees, horizontal tail leading edge
vtail_area              = 131.32                 //Square feet
vtail_span              = 13.5                  //Feet, tip to body
vtail_sweep             = 42.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -39.0                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 8.1                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 71.69                  //Square feet
aileron_area            = 65.23                  //Square feet
rudder_area             = 61.61                  //Square feet
elevator_up_limit       = 29.0                  //Degrees
elevator_down_limit     = 19.9                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 20.0                  //Degrees
rudder_limit            = 26.0                  //Degrees
elevator_trim_limit     = 20.0                  //Degrees
spoiler_limit           = 52.0                  //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
stick_shaker=1

[Reference Speeds]
flaps_up_stall_speed=162.0                 //Knots True (KTAS)
full_flaps_stall_speed=134.0                 //Knots True (KTAS)
cruise_speed=1035                 //Knots True (KTAS)
max_mach                = 1.85
max_indicated_speed     = 2000                   //Red line (KIAS)

[stall_warning]
type=2

[TailHook]
tailhook_length=4
tailhook_position = -15.0, 0.0, -1.0
cable_force_adjust = 1.0

[folding_wings]
wing_fold_system_type=4
fold_rates=30,30

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[deice_system]
structural_deice_type=0