[fltsim.0]
title=Mil Mi-1
sim=Mi-1
model=
panel=
sound=
texture=
prop_anim_ratio=-1.76
atc_id_color=
atc_id=CCCP-010
ui_manufacturer=Mil
ui_type=Mi-1
ui_variation="ДОСААФ"
description="Russian helicopters Mil Mi-1. "


[General]
atc_type=Mil
atc_model=Mi-4
performance="Maximum Speed\n170 km/hr\n\nCruise Speed\n145 km/hr\n\nEngine\nProgress AI-82V, 1700 hp\n\nMaximum Range\n600 km\n\nService Ceiling\n3000 m\n\nHovering Ceiling\n1220 m\n\nFuel Capacity\nXXX L\n\nEmpty Weight\n1880 kg\n\nMax Gross Weight\n2550 kg\n\nLength\n12.1 m\n\nRotor Span\n14.35 m\n\nHeight\n3.3 m\n\nSeating\n1+2"
editable=0


[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=1500.000
empty_weight_roll_MOI=9000.000
empty_weight_pitch_MOI=13000.000
empty_weight_yaw_MOI=11500.000
empty_weight_coupled_MOI=1200.000
max_gross_weight=2100.000
CG_forward_limit=0.000
CG_aft_limit=1.000


;Moments of Inertia
empty_weight_pitch_MOI   =  6000
empty_weight_roll_MOI    =  4000
empty_weight_yaw_MOI     = 10000
empty_weight_coupled_MOI =     0

[contact_points]
point.0=1.000000,33.333333,0.000000,-9.366667,3003.698634,0.000000,0.520132,54.000000,1.120889,2.500000,1.260614,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-8.333333,-8.333333,-9.200000,3003.698634,1.000000,0.520132,0.000000,1.002901,2.500000,1.416001,8.000000,8.000000,2.000000,0.000000,0.000000
point.2=1.000000,-8.333333,8.333333,-9.200000,3003.698634,2.000000,0.520132,0.000000,1.002901,2.500000,1.416001,9.000000,9.000000,3.000000,0.000000,0.000000

static_pitch=2.3
static_cg_height=6.0
gear_system_type=0

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 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



 
        //0  Class                        <0=none,1=wheel, 2=scrape, 3=skid>
        //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)

[contact_points]
static_pitch = 0.0
static_cg_height = 0.0
gear_system_type = 0
max_number_of_points = 4



[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.0  //Brake scalar

[hydraulic_system]
normal_pressure = 0.0    //PSI

[pViews]
eyepoint = -2.75,  -2.20, 0.95



[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 0
Com.2         = 0
Nav.1         = 0
Nav.2         = 0
Adf.1         = 1
Transponder.1 = 0
Marker.1      = 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.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000

[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=2,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt

[fuel]
Center1  = -2.93, 0.0, -1.38, 66.00, 0.0         //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 1.55, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum	 -8.5, 0.0, 0.0
fuel_flow_scalar= 1.0                           //Fuel flow scalar
min_throttle_limit =  0.0;                      //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
cylinder_displacement=91.67 
compression_ratio=8.0 
number_of_cylinders=12 
max_rated_rpm=2700.0 
max_rated_hp=280.0
fuel_metering_type=0 
cooling_type=0 
normalized_starter_torque=0.3 
turbocharged=1 
max_design_mp=0.0 
min_design_mp=1.0 
critical_altitude=0.0 
emergency_boost_type=0 
emergency_boost_mp_offset=0.0 
emergency_boost_gain_offset=0.0 
fuel_air_auto_mixture=0 
auto_ignition=0 
max_rpm_mechanical_efficiency_scalar=1.0 
idle_rpm_mechanical_efficiency_scalar=1.0 
max_rpm_friction_scalar=1.0 
idle_rpm_friction_scalar=1.0 

[Reference Speeds]
cruise_speed            = 76.0                 //Knots True (KTAS) 90.0
max_indicated_speed     = 100                  //Red line (KIAS) 102

[autopilot]
autopilot_available= 0
flight_director_available= 0

[yaw_string]
yaw_string_available=1

[Helicopter]
reference_length       = 39.65   	
reference_frontal_area = 17.7	
reference_side_area    = 47.07 	
side_aero_center       = -10.82		
right_trim_scalar      =1.0
correlator_available   = 1
governed_pct_rpm_ref   = 1.04
governor_pid = 0.4, 0, 0.1, 0, 0.2
rotor_brake_scalar     = 1.0
torque_scalar          = 1.0
cyclic_roll_control_scalar  =1.0
cyclic_pitch_control_scalar =1.0
pedal_control_scalar        =1.0
collective_on_rotor_torque_scalar = 1.0

[fuselage_aerodynamics]
drag_force_cf      = 3.15		
side_drag_force_cf = 10.0		
pitch_damp_cf      = -10.0		
roll_damp_cf       = -5.0		
yaw_damp_cf        = -5.0		
yaw_stability_cf   = 0.27		

[MainRotor]
Position =0.1, 0.0, 9.805                       //Longitudinal, Lateral, Vertical feet from datum  0.0, -0.15, 6.905
Radius   = 23.583                               //feet  
max_disc_angle = 5.0
RatedRpm = 205			
Number_of_blades = 3
Weight_per_blade = 20.0		
Weight_to_moi_factor = 0.58		
inflow_vel_reference = 34.0

[SecondaryRotor]
Position = -28.48, -1.21, 5.524                    //Longitudinal, Lateral, Vertical feet from datum
TailRotor = 1
Radius   = 4.101                                 //feet

[Views]
eyepoint=0.000000,0.000000,0.000000

[propeller]
thrust_scalar=1.0 
propeller_type=1 
propeller_diameter=54.16 
propeller_blades=5 
propeller_moi=6.9 
beta_max=45.0 
beta_min=15.2 
min_gov_rpm=1100.0 
prop_tc=0.1 
gear_reduction_ratio=1.0 
fixed_pitch_beta=0.0 
low_speed_theory_limit=24.0 
prop_sync_available=0 
prop_deice_available=0 
prop_feathering_available=1 
prop_auto_feathering_available=0 
min_rpm_for_feather=700.0 
beta_feather=82.5 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=0.0 
minimum_on_ground_beta=0.0 
minimum_reverse_beta=0.0