[fltsim.0]
title=Mi-4A VVS
sim=Mi-4A VVS
model=
panel=
sound=
texture=
kb_checklists=
prop_anim_ratio=-0.90
atc_id=Mi-4A VVS
atc_model=Mi-4A VVS
ui_manufacturer=MIL
ui_type=Mi-4A VVS
ui_variation=Mi-4A VVS
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[General]
atc_type=HELICOPTER 
performance=Data:\nLenght (rotors turning): 25,4 m ( 83,3 ft )\nLenght (fuselage): 18,4 m ( 60,3 ft )\nHeight: 5,7 m ( 18,7 ft ) \nWitdth: 2,5 m ( 8,8 ft )\nMain rotor diameter: 21,3 m \/ 5 \/ ( 69,9 ft )\nTail Rotor diameter: 3,9 m \/ 3 \/ ( 12,8 ft )\nWeight: - Max gross: 13.000 kg ( 28668 lb ), Normal takeoff: 11.000 kg ( 24250 lb ), Emty:7.088-7.370 kg ( es. 15700 lb ) \nEngine: 2x1637 KW ( 2200 shp ) TV3-117VM turboshaft\nFuel: - Consumotion: 445 l ( 117 gal ) Port: 745 l ( 197 gal) Starboard: 680 l ( 749 gal )\nSpeed: - Maximum: 250 km\/h ( 135 knots ), Cruising: 240 km\/h ( 129 knots ) Ceiling: - Service: 5000-5700 m ( 16400-18700), Hover ( out of grnd effect ): 1760 m ( 5770 ), Hover ( in grnd effect ): 1900-3900 ( 6230- 12800 )\nClimb rate: 9 m\/s ( 30 ft\/s )\nPayload: - Internal: 4000 kg ( 8800 lb) External: 3000 kg ( 6600 lb )\n\n   \n 
atc_model=MI 8 
//=================================================
editable=0 

[weight_and_balance]

// ACM V2.3
max_gross_weight = 26000
empty_weight = 15553
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 7.708, 0, 0
empty_weight_pitch_MOI = 123644
empty_weight_roll_MOI = 38451
empty_weight_yaw_MOI = 110966
empty_weight_coupled_MOI = 0
max_number_of_stations = 2

station_load.0 = 170, 3.96, -1.29, 3.29
station_load.1 = 170, 3.98, 1.44, 3.22


[lights]

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

light.0 = 5, 12.71, 0.48, -1.28, fx_ES_3d-lights_brown
light.1 = 4, 5.11, 0, 3.06, fx_vclight14
light.2 = 3, 6.52, -3.32, -1.32, fx_navred
light.3 = 3, 6.51, 3.35, -1.32, fx_navgre

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 5.100
engine.0 = 5.6, 0, 0,
min_throttle_limit=0.000000

[smokesystem]
smoke.0 = -3.48, 10.19, -2.73, fx_engstrt
smoke.1 = -3.48, 10.18, 2.75, fx_engstrt

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_mi-8,1
waterrotorwash = fx_rtr_wt
startup = fx_b25_startup4

[fuel]

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

fuel_type = 1
number_of_tank_selectors = 2

Center1 = 0.1, -0.05, 1.5, 117, 0
electric_pump=0


[contact_points]
static_pitch = -0.2
static_cg_height = 7.6
tailwheel_lock = 0
max_number_of_points = 4

point.0 = 1, 9.2796, 5, -7.5064, 1600, 0, 0.676, 90, 0.3, 1.3, 0.95, 0, 0, 3, 0, 0
point.1 = 1, 9.2796, -5, -7.5064, 1600, 0, 0.676, 90, 0.3, 1.3, 0.95, 0, 0, 3, 0, 0
point.2 = 1, -2.9793, -8.6, -7.4265, 1600, 1, 1.156, 0, 0.3, 1.3, 0.95, 0, 0, 1, 0, 0
point.3 = 1, -2.9781, 8.6, -7.4266, 1600, 2, 1.156, 0, 0.3, 1.3, 0.95, 0, 0, 2, 0, 0


[keyboard_response]
elevator = 100.000000, 180.000000
aileron = 200.000000, 1000.000000
rudder = 200.000000, 1000.000000


[forcefeedback]

[airplane_geometry]
//ACM_AREAW1// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAW2// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAW3// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAW4// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH1// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH2// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH3// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAH4// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV1// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV2// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV3// 0,0,0,0,0,0,0,0,0,0
//ACM_AREAV4// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW1// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW2// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW3// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAW4// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH1// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH2// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH3// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAH4// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV1// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV2// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV3// 0,0,0,0,0,0,0,0,0,0
//ACM_CAREAV4// 0,0,0,0,0,0,0,0,0,0
wing_winglets_flag = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 150
electric_always_available = 0
autopilot = 4, 4, 15
avionics = 0, 5, 15
pitot_heat = 4, 2, 15
additional_system = 0, 2, 15
marker_beacon = 4, 2, 10
fuel_pump = 0, 5, 17
starter1 = 0, 20, 24
starter2 = 0, 20, 24
starter3 = 0, 20, 24
light_nav = 0, 5, 10
light_beacon = 4, 5, 15
light_landing = 4, 5, 15
light_taxi = 0, 5, 15
light_strobe = 0, 5, 10
light_panel = 0, 5, 10
hydraulic_pump = 0, 5, 15
fuel_transfer_pump = 0, 5, 15
light_recognition = 4, 5, 10
light_logo = 4, 5, 10

[flight_tuning]
rudder_effectiveness=0.05 
aileron_effectiveness=1.0 
elevator_effectiveness=1.3 
//=================================================

[brakes]
parking_brake = 1      //Parking brake available
toe_brakes_scale = 0.4  //Brake scalar
//=================================================
[hydraulic_system]
normal_pressure=797.700
engine_map=1,0,0,0
electric_pumps=1
//=================================================
[Views]
eyepoint=3.1, -1.50, 4.45 
//=================================================

[exits]
number_of_exits=4
exit_rate.0=0.4                                                           
exit_rate.1=0.4      
exit_rate.2=0.4
exit_rate.3=0.4
//=================================================

[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 
//=================================================

[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=2,0 
//=================================================

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2 
//=================================================
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
//=================================================
[TailHook]
tailhook_length=1                             ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.3
[folding_wings]
wing_fold_system_type=4			;0=None
fold_rates=0.12,0.11				;Percent per second
[TurbineEngineData]
fuel_flow_gain=0.002 
inlet_area=4.772 
rated_N2_rpm=15000.000 
static_thrust=2225.000 
afterburner_available=0 
reverser_available=0.000 
//=================================================

[Reference Speeds]
cruise_speed=85.0                 //Knots True (KTAS)
max_indicated_speed     = 115.0                   //Red line (KIAS)
//=================================================

[fuselage_aerodynamics]
drag_force_cf=0.000000
side_drag_force_cf=0.000000
pitch_damp_cf=1.500000
roll_damp_cf=1.000000
yaw_damp_cf=0.600000
yaw_stability_cf=2.500000
//=================================================
[MainRotor]
Position = 7.873, 0, 6.561
Radius = 34.931
max_disc_angle = 4.0
Number_of_blades = 5
weight_per_blade = 264.0
Weight_to_moi_factor = 42.0
inflow_wel_reference =43.0
inflow_vel_reference=0.000000
 //=================================================
[SecondaryRotor]
TailRotor = 1
Position = -34.776, 2.378, 4.101
Radius = 6.397 
//=================================================
[autopilot]
autopilot_available=1 
flight_director_available=0 
attitude_indicator= 0
direction_indicator=0
default_pitch_mode=1
max_pitch=20.0
max_pitch_acceleration=5.0
default_vertical_speed=0.01 
default_bank_mode=2
max_bank=30
max_bank_acceleration=1.5
autothrottle_available=0 
pitch_takeoff_ga=8.000 
max_pitch_velocity_lo_alt= 5.000
max_pitch_velocity_hi_alt= 5.500
max_pitch_velocity_lo_alt_breakpoint= 20000.000
max_pitch_velocity_hi_alt_breakpoint= 28000.000
max_bank_velocity= 5.000
max_throttle_rate= 0.100
nav_proportional_control= 9.000
nav_integrator_control= 0.250
nav_derivative_control= 0.000
nav_integrator_boundary= 2.500
nav_derivative_boundary= 0.000
gs_proportional_control= 9.520
gs_integrator_control= 0.260
gs_derivative_control= 0.000
gs_integrator_boundary= 0.700
gs_derivative_boundary= 0.000
yaw_damper_gain= 5.000
//=================================================

[yaw_string]
yaw_string_available=1
//=================================================
[helicopter] 
right_trim_scalar=-5.0
cyclic_roll_control_scalar  =1.0
cyclic_pitch_control_scalar =1.0