[fltsim.0]
title=Samdim Design Tu-95MS
sim=Tu95MS
model=95
panel=95
sound=95
texture=95
checklists=
atc_id=MS10
atc_airline=VVS
atc_flight_number=M10
ui_manufacturer=Tupolev
ui_type=Tu-95MS
ui_variation=010
description=TUPOLEV TU-95MS. strategic bomber and missile carrier \nSamdim Design (c) 2008
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[fltsim.1]
title=Samdim Design Tu-142M
sim=Tu95MS
model=142
panel=95
sound=95
texture=142
checklists=
atc_id=MS10
atc_airline=VVS
atc_flight_number=M10
ui_manufacturer=Tupolev
ui_type=Tu-142M
ui_variation=089
description=TUPOLEV TU-142M. maritime reconnaissance and anti-submarine aircraft \nSamdim Design (c) 2008
atc_id_font=Verdana,-11,1,600,0

[General]
atc_type=TU95MS 
atc_model=TU95MS 
performance=See Flight Manual 

editable=0
[weight_and_balance]

// ACM V2.5
max_gross_weight = 407852
empty_weight = 205029
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -5, 0, 0
empty_weight_pitch_MOI = 5600000
empty_weight_roll_MOI = 0
empty_weight_yaw_MOI = 6400000
empty_weight_coupled_MOI = 0
CG_forward_limit = 0
CG_aft_limit = 1
max_number_of_stations = 1

station_load.0 = 0,0,0,0


[lights]

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

light.0 = 2, -52.93, -0.02, -5.63, fx_strobe
light.1 = 2, -36.79, -1.00, 3.05, fx_strobe
light.2 = 3, -93.37, 0, -1.39, fx_navwhi
light.3 = 3, 25.35, -1.01, 2.95, fx_navwhi

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 0.38
min_throttle_limit = -0.22
engine.0 = 18, -40.8,0
engine.1 = 29, -21.2,-2
engine.2 = 29, 21.2,-2
engine.3 = 18, 40.8,0

[smokesystem]
smoke.0 = 38,-13.3,-40.8,Fx_95smok
smoke.1 = 38,-13.3,-21,Fx_95smok
smoke.2 = 38,-13.3,21,Fx_95smok
smoke.3 = 38,-13.3,40.8,Fx_95smok

[effects]
windshield_rain_effect_available = 1

[fuel]

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

fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 0

Center1 = -27.8, 0, 0, 1645, 400
Center2 = 8.2, -2.3, 2, 1448, 400
Center3 = 8.2, 2.3, 2, 1448, 400
LeftMain = 1.8, -22, 0.4, 5069, 400
LeftAux = -12.8, -39, -0.5, 2566, 400
LeftTip = -27.8, -63, -1.5, 1612, 400
RightMain = 1.8, 22, 0.4, 5069, 400
RightAux = -12.8, 39, -0.5, 2566, 400
RightTip = -27.8, 63, -1.5, 1612, 400
External1 = 5.5, -9, 1.5, 2435, 400
External2 = 5.5, 9, 1.5, 2435, 400


[contact_points]
static_pitch = 0.6
static_cg_height = 17.1
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 8

point.0 = 1,  42,      0, -17.50, 1300.0, 0, 1.73, 60, 0.636, 1.938, 0.7,  18, 18, 0, 390, 400
point.1 = 1, -9.0971, -21, -16.4414, 2000, 1, 2.46, 0, 1.19, 1.372, 0.9, 30, 31, 2, 390, 400
point.2 = 1, -9.0986, 21, -16.4428, 2000, 2, 2.46, 0, 1.19, 1.372, 0.9, 31, 32, 3, 390, 400
point.3 = 2, -91.6231, 0, -2.3157, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.4 = 2, 53.3451, 0, -6.1149, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.5 = 5, -36.5447, -0.1456, -3.9563, 1600, 0, 0, 50, 0, 0, 1, 8, 8.2, 0, 0, 0
point.6 = 2, -37.9626, -83.5335, -3.4621, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.7 = 2, -37.6394, 83.1222, -3.4621, 0, 0, 0, 0, 0, 0, 0, 0, 0, 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// 0,0,0,8.4795,2.7889,2.7889,1.9528,10.0083,5.5778,5.5778
//ACM_AREAW2// 3.9056,11.5372,8.3667,8.3667,5.8584,13.0660,11.1556,11.1556,7.8112,14.5949
//ACM_AREAW3// 13.9445,13.9445,9.7641,16.1237,16.7335,16.7335,11.7169,17.6526,19.5224,19.5224
//ACM_AREAW4// 13.6697,19.1814,22.3113,22.3113,15.6225,20.7103,25.1002,25.1002,17.5754,22.2391
//ACM_AREAH1// 0,0,0,5.7912,0.9652,0.9652,0.8098,6.3115,1.9304,1.9304
//ACM_AREAH2// 1.6197,6.8318,2.8956,2.8956,2.4296,7.3522,3.8608,3.8608,3.2395,7.8725
//ACM_AREAH3// 4.8260,4.8260,4.0494,8.3928,5.7912,5.7912,4.8593,8.9132,6.7564,6.7564
//ACM_AREAH4// 5.6692,9.4335,7.7216,7.7216,6.4791,9.9539,8.6868,8.6868,7.2890,10.4742
//ACM_AREAV1// 0,0,0,7.5590,0.8398,0.8398,0.6898,7.6442,1.6797,1.6797
//ACM_AREAV2// 1.3797,7.7293,2.5196,2.5196,2.0696,7.8145,3.3595,3.3595,2.7595,7.8997
//ACM_AREAV3// 4.1994,4.1994,3.4494,7.9849,5.0393,5.0393,4.1393,8.0700,5.8792,5.8792
//ACM_AREAV4// 4.8292,8.1552,6.7191,6.7191,5.5191,8.2404,7.5590,7.5590,6.2090,8.3255
//ACM_CAREAW1// 12.5501,12.5501,13.0274,14.7233,13.9445,13.9445,14.0038,15.6149,15.3390,15.3390
//ACM_CAREAW2// 14.9802,16.5066,16.7335,16.7335,15.9567,17.3982,18.1279,18.1279,16.9331,18.2898
//ACM_CAREAW3// 19.5224,19.5224,17.9095,19.1814,20.9168,20.9168,18.8859,20.0730,22.3113,22.3113
//ACM_CAREAW4// 19.8623,20.9646,23.7058,23.7058,20.8387,21.8563,25.1002,25.1002,21.8151,22.7479
//ACM_CAREAH1// 0,0,2.8956,5.7912,0.9652,0.9652,3.7054,6.4563,1.9304,1.9304
//ACM_CAREAH2// 4.5153,7.1214,2.8956,2.8956,5.3252,7.7865,3.8608,3.8608,6.1351,8.4516
//ACM_CAREAH3// 4.8260,4.8260,6.9450,9.1167,5.7912,5.7912,7.7549,9.7819,6.7564,6.7564
//ACM_CAREAH4// 8.5648,10.4470,7.7216,7.7216,9.3747,11.1121,8.6868,8.6868,10.1846,11.7772
//ACM_CAREAV1// 0,0,1.8897,5.6692,0.8398,0.8398,2.5796,6.0568,1.6797,1.6797
//ACM_CAREAV2// 3.2695,6.4443,2.5196,2.5196,3.9594,6.8318,3.3595,3.3595,4.6493,7.2194
//ACM_CAREAV3// 4.1994,4.1994,5.3392,7.6069,5.0393,5.0393,6.0291,7.9944,5.8792,5.8792
//ACM_CAREAV4// 6.7190,8.3820,6.7191,6.7191,7.4089,8.7695,7.5590,7.5590,8.0988,9.1570
wing_area = 3120
wing_span = 164.69
wing_root_chord = 27.81
wing_dihedral = -2.5
wing_incidence = 1
wing_twist = -1
oswald_efficiency_factor = 1.05
wing_winglets_flag = 0
wing_sweep = 35
wing_pos_apex_lon = 27.5
wing_pos_apex_vert = 0
htail_area = 592
htail_span = 57
htail_pos_lon = -78.16
htail_pos_vert = -2
htail_incidence = 1.0
htail_sweep = 40
vtail_area = 438
vtail_span = 24.79
vtail_sweep = 39.40
vtail_pos_lon = -92
vtail_pos_vert = -12.57
elevator_area = 146
aileron_area = 143
rudder_area = 115
elevator_up_limit = 28
elevator_down_limit = 17
aileron_up_limit = 28
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 60
spoiler_limit = 50
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1,1,1
electric_always_available = 1
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 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

[TurbineEngineData]
fuel_flow_gain=0.018 
inlet_area=1.0 
rated_N2_rpm=8450 
static_thrust=156 
afterburner_available=1 
reverser_available=1 

[turboprop_engine]
power_scalar=1.0 
maximum_torque=72600     ;H:maximum_torque(72600)

[propeller]
thrust_scalar=1.0                   //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=18.368                 //Propeller Diameter, (feet)
propeller_blades=8                     //Number of propeller blades
propeller_moi=530                //Propeller moment of inertia
beta_max=21.4  //21.4              //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=6     //8               //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=8450     //25520            //Miminum governed RPM
prop_tc=0.008                 //Prop time-constant
gear_reduction_ratio=11.3     //15.4                  //Propeller gear reduction ratio
fixed_pitch_beta=0                    //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=8                   //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1                     //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1                     //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=700                   //Minimum RPM for prop feathering
beta_feather=91                  //Feathering pitch angle (degrees)
power_absorbed_cf=0.95                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-0.0001 
                 //Minimum pitch angle in reverse, (degrees)

[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=2.0 
pitch_stability=1.0 
roll_stability=1.1 
yaw_stability=1.1 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 

[Reference Speeds]
flaps_up_stall_speed=175.0 
full_flaps_stall_speed=132.0 
cruise_speed=370.0 
max_indicated_speed=400.0
max_mach=0.82

[flaps.0]
type=1
span-outboard=0.8
extending-time=37
flaps-position.0=0
flaps-position.1=10
flaps-position.2=20
flaps-position.3=27
flaps-position.4=35
flaps-position.5=45
damaging-speed=250
blowout-speed=300
lift_scalar=0.7
drag_scalar=0.5   /0.7
pitch_scalar=0.7
system_type=1
//[flaps.1]
type=1
span-outboard=0.8
extending-time=37
flaps-position.0=0
flaps-position.1=0
flaps-position.2=0
flaps-position.3=0
flaps-position.4=35
flaps-position.5=45
damaging-speed=200
blowout-speed=250
lift_scalar=0.3
drag_scalar=0.6   /0.8
pitch_scalar=0.5  /0.6
system_type=1
333[exits]
number_of_exits=4
exit_rate.0=0.4
exit_rate.1=0.4
exit_rate.2=0.4
exit_rate.3=10000

[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1 
Transponder.1=1 
Marker.1=1 

[Views]
eyepoint=1.550, -1.00, 0.950 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=80 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8 
use_no_default_bank=1
use_no_default_pitch=1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=2.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=2.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000
default_pitch_mode=0
default_bank_mode=0

[direction_indicators]
direction_indicator.0=3,0 

[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_idle=5.042029
flap_limit_power=25.496622
[brakes]
toe_brakes_scale=0.48
parking_brake=1
[hydraulic_system]
normal_pressure=3000.000000
electric_pumps=0
engine_map=1,1,1,1
[stall_warning]
type=1
[pitot_static]
vertical_speed_time_constant=1

[TailHook]
tailhook_length=1
tailhook_position=0,0,0,
cable_force_adjust=0.00001
[folding_wings]
wing_fold_system_type=4
fold_rates=0.20