//// Mil Mi-8T/MT - 2010 - Vladimir Zhygulskiy  - all right reserved

//=================================================:

[fltsim.0]
title=Mil Mi-8MT Russian Ministry of Emergency  (MChS)
sim=Mi8zh
model=PZU
panel=
sound=
texture=PZU
checklists=
kb_checklists=
kb_reference=
atc_id=RF23
atc_airline=MChS
atc_flight_number=RF23
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=MChS
visual_damage=1 
description=Mil Mi-8MTV  transport - SAR helicopter, Russia. 
atc_heavy=0

\\\================================

[fltsim.1]
title=Mil Mi-8MTV Russian Army
sim=Mi8zh
model=NURS
panel=
sound=
texture=NURS
checklists=
kb_checklists=
kb_reference=
atc_id=RA57
atc_airline=Ru Army
atc_flight_number=RA57
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=Russian Army
visual_damage=1 
description=Mil Mi-8MT multirole helicopter modern Russian Army. 
atc_heavy=0

\\\================================

[fltsim.2]
title=Mil Mi-8MT VVS Afganistan War
sim=Mi8zh
model=EVU
panel=AFG
sound=
texture=AFG
checklists=
kb_checklists=
kb_reference=
atc_id=BS31
atc_airline=VVS
atc_flight_number=BS31
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=Soviet AF (VVS) 262 Bagram squadron
visual_damage=1 
description= Вечная память!..  We remember. Eternal memory... Mil Mi-8MT military transport helicopter Soviet AF (VVS) of time Afganistan War (1979-1989) - 262 Bagram helicipters squadron, USSR. 
atc_heavy=0

\\\================================
[fltsim.3]
title=Mil Mi-8MT Kolavia
sim=Mi8zh
model=NORD
panel=
sound=
texture=NORD
checklists=
kb_checklists=
kb_reference=
atc_id=RA77
atc_airline=Clavia
atc_flight_number=RA77
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=Kolavia
visual_damage=1 
description=Mil Mi-8MT transport helicopter  with  External load (oil truss), Kolavia AL, oil worksite in  much-much Nord of Russia .
atc_heavy=0
\\================================

[fltsim.4]
title=Mil Mi-8MT UN
sim=Mi8zh
model=UN
panel=
sound=
texture=UN
checklists=
kb_checklists=
kb_reference=
atc_id=URHL
atc_airline=UN
atc_flight_number=URHL
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=UN
visual_damage=1 
description=Mil Mi-8MT transport helicopter  UN (Kherson helicopters brigade, based in Kherson AB (UKOH), South Ukraine).
atc_heavy=0
\\================================

[fltsim.5]
title=Mil Mi-8MT Aeroflot
sim=Mi8zh
model=GVF
panel=
sound=
texture=GVF
checklists=
kb_checklists=
kb_reference=
atc_id=RA2585
atc_airline=Aeroflot
atc_flight_number=RA2585
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=Aeroflot
visual_damage=1 
description=Mil Mi-8MT transport helicopter  Aeroflot AL, Russia.
atc_heavy=0
\\================================

[fltsim.6]
title=Mil Mi-8MT Ukraine NAVI
sim=Mi8zh
model=NURS
panel=
sound=
texture=UA
checklists=
kb_checklists=
kb_reference=
atc_id=UA09
atc_airline=Ua NAVI
atc_flight_number=UA09
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=UA NAVI
visual_damage=1 
description=Mil Mi-8MT transport helicopter  Ukraine NAVI.
atc_heavy=0
\\\=================================

[General]
atc_type=Mil Mi-8
performance=Mil Mi-8MT, medium multirole helicopter. Version 2010. Autur -VLadimir Zhyhulskiy, former sergeant  Soviet AF, Kiev, Ukraine.


//////////////=============================

[weight_and_balance]
max_gross_weight = 26000    \\\\26000
empty_weight = 15500               \\\16000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.0, 0, 0
empty_weight_pitch_MOI =30500
empty_weight_roll_MOI =30500          \\\\12500
empty_weight_yaw_MOI =67000   \\\\100000   \\\19000
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = "210, 6, 1.2, 0, Pilot"
station_load.1 = "210, 6,-1.2, 0, Co Pilot"

////================================================
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type =1
Engine.0            =  10.0,  5.3, 3.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1            = 10.0, -5.3, 3.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 130.0
engine.0 = 0, 0, 4 
min_throttle_limit=0.000000

[turboprop_engine]
power_scalar = 0.7

[TurbineEngineData]
fuel_flow_gain=0.1 
inlet_area=15.11 
rated_N2_rpm=41.36 
static_thrust=500.000 
afterburner_available=0 
reverser_available=0.000 

////================================================
[propeller]
propeller_type=1
thrust_scalar =0.7
propeller_diameter=6.883000
propeller_blades=2
propeller_moi=5.706520
beta_max=0.000000
beta_min=15.000000
min_gov_rpm=0.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

////================================================
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
Center1 =  -3.0, 0,  -4, 740, 20
LeftAux =  -3.0, -3,  -4, 240, 20
RightAux=  -3.0, 3,  -4, 240,  20
electric_pump=0

////================================================
[flight_tuning]
cruise_lift_scalar=0.9
parasite_drag_scalar=1.15
induced_drag_scalar=1.0
rudder_effectiveness=0.05           \\\0.05
aileron_effectiveness= 1.0
elevator_effectiveness=1.0

////================================================
////================================================
////================================================

[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)

static_pitch = 3.4
static_cg_height = 6.5
max_number_of_points = 8

//--------0-----1------2-------3-----4---5---6-----7----8------9---10----11-12-13-14--15
	     	
point.0 = 1,   12.22, 0.00, -7.45, 2500, 0, 0.55, 45, 0.52, 1.25, 0.5,  0, 0, 2, 00, 300 ; nose wheel left
point.1 = 1,  -8.00, -10.90, -6.58, 2500, 1, 0.70,  0,  0.80, 1.25, 0.5,  0, 0, 3, 00, 300 ; aft wheel left
point.2 = 1,  -8.00,  10.90, -6.58, 2500, 2, 0.70,  0,  0.80, 1.25, 0.5,  0, 0, 3, 00, 300 ; aft wheel right
point.3 = 2,   6.60,  0.00, -2.47, 2500, 0, 0.00,  0,  0.0,   0.0, 0.0,  0, 0, 5, 0,  0   ; scrape fuse front
point.4= 2,  -8.50,  0.00, -2.28, 2500, 0, 0.00,  0,  0.0,   0.0, 0.0,  0, 0, 6, 0,  0   ; scrape fuse aft
point.5 = 2, -31.40,  0.00,  4.43, 2500, 0, 0.00,  0,  0.0,   0.0, 0.0,  0, 0, 9, 0,  0   ; scrape boom
point.6 = 5,   0.00,  0.00,  0.00,    0, 0, 0.00,  0., 0.0,   0.0, 0.0,  1, 1, 0, 0,  0   ; Water rudder

gear_system_type=0

////================================================
////================================================
////================================================


[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1,  -21.20,  0.00,  5.30,  fx_beacon   ; Beacon top
light.1 = 4,   5.00,  0.00,  1.30,  fx_vclight    ; Pilots
light.2 = 4,   4.00,   -1.00,  1.7,  fx_vclight    ; Pilots
light.3 = 4,   4.00,   1.00,  1.7,  fx_vclight    ; Pilots
Light.4= 10, -10.00, 0.00, 2.50, ZH_M8cabin


////================================================
////==================EFFECT&ANIMATIONS================
////================================================

[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 = 1
fold_rates =  0.4, 0.4

[exits]
number_of_exits=2
exit_rate.0=0.3
exit_rate.1=0.7

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete =ZH_zero
touchdown=ZH_zero

[SMOKESYSTEM]
smoke.0=0.00, -15.30, 0.00, ZH_ikpp.fx     /// 1 click-5 second!
smoke.1=-0.00,7.00,10.00, ZH_nurs        /// 1 click-1 missile!
smoke.2=0.00,7.00,-10.00, ZH_nurs       /// 1 click-1 missile!
smoke.3=0.00, 20.00, 0.0, ZH_PKT       /// 1 click-5 second!

[anemometers]
anemometer.0 = -10.0, 0.0, 2.7       //Position from Datum

////================================================
////================================================
[Views]
eyepoint=1.61, -2.1, 2.2
////================================================
////================================================

//===================HELI==========================
[MainRotor]
Position = 9.873, 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 

[helicopter] 
low_realism_stability_scale = 1.35, 1.3, 5.0             //Pitch , Bank, Yaw Scalars on Stability in Low Realis
right_trim_scalar=-5.0
cyclic_roll_control_scalar  =1.0
cyclic_pitch_control_scalar =1.0
//=================================================

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.000000 
autothrottle_available=0 
pitch_takeoff_ga=8.000000 
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
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=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
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=0.000000
///================================================

[brakes]
toe_brakes_scale=1.17
parking_brake=1
///================================================


///==================OTHER===========================
[electrical]
;BusType, MaxAmpLoad, MinVoltage       
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 180
electric_always_available = 1
gear_motor        = 0, 5, 17
autopilot         = 0, 5, 17
avionics_bus      = 0, 10, 17
avionics          = 1, 5, 17
pitot_heat        = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon     = 0, 2, 17
gear_warning      = 0, 2, 17
fuel_pump         = 0, 5, 17
starter1          = 0, 20, 17
light_nav         = 0, 3, 17
light_beacon      = 0, 3, 17
light_landing     = 0, 5, 17
light_taxi        = 0, 5, 17
light_strobe      = 0, 3, 17
light_panel       = 0, 2, 17


[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1 
Com.2=1
Nav.1=1, 0, 1 
Nav.2=1 
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=3,0 

[Reference Speeds]
cruise_speed            =125.0                 //Knots True (KTAS)
max_indicated_speed     =135.0		     //Knots True (KTAS)

[hydraulic_system]
normal_pressure=0.0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[keyboard_response]
elevator = 100, 130
aileron  = 100, 130
rudder   = 100, 130

[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000