[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. "

[fltsim.1]
title=Mil Mi-1 MOSKVICH
sim=Mi-1
model=
panel=
sound=
texture=1
prop_anim_ratio=-1.76
atc_id_color=
atc_id=CCCP-40396
ui_manufacturer=Mil
ui_type=Mi-1
ui_variation="Москвич"
description="Russian helicopters Mil Mi-1. "


[General]
atc_type=Mil
atc_model=Mi-1
performance="Maximum Speed\n170 km/hr\n\nCruise Speed\n145 km/hr\n\nEngine\nProgress AI-26V, 580 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]
max_gross_weight = 5622                          // (pounds) 1370	//5622	
empty_weight = 4189                             // (pounds) 862.4  	//4189

reference_datum_position     =   0.0,   0.0, 0.0   // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  0.0,  0.0, 0.0   // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 3

station_load.0 = "160, 6.905,  0.0, 0.0, Pilot"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "180, 4.66, -1.03, -0.9, Passenger"      // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "180, 4.66, 1.03, -0.9, Passenger"      // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


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

point.0=1,   8.976,    0.0,  -4.98,  2000,  0,  0.50, 180,   0.20, 1.40, 0.95, 0, 0, 0, 0, 0
point.1=1,  -1.553,   -5.35,  -4.93,  3000,  1,  0.60,   0,   0.25, 1.60, 0.95, 0, 0, 0, 0, 0
point.2=1,  -1.553,    5.35,  -4.93,  3000,  2,  0.60,   0,   0.25, 1.60, 0.95, 0, 0, 0, 0, 0

point.3=2,  -23.823,    0.0,  -1.6,  1000,  0,  0,   0.0,   0.00, 0.00, 0.00, 0, 0, 9, 0, 0
point.4=2,    2.2,    0.0,  -1.0,  1400,  0,  0,   0.0,   0.00, 0.00, 0.00, 0, 0, 9, 0, 0

point.5=2,   0.0,  -24.0,   5.5,   0.0,  0,  0,   0.0,   0.00, 0.00, 0.00, 0, 0, 5, 0, 0
point.6=2,   0.0,   24.0,   5.5,   0.0,  0,  0,   0.0,   0.00, 0.00, 0.00, 0, 0, 6, 0, 0

static_pitch=0.33
static_cg_height=4.75
gear_system_type=0

[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 8.63, -1.99, -1.80,  fx_navred ,
light.1 = 3, 8.63,  1.99, -1.80,  fx_navgre ,
light.2 = 3, -12.08,  0.40, 2.20,  fx_navwhi,
light.3 = 1, -12.08,  0.01, 0.30,  fx_beacon,
light.4 = 5, 8.976, 0.00,  -2.20, -1.65,  fx_landing,


[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]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 90.0                     //Cubic inches per cylinder
compression_ratio= 8.5                          //Compression ratio
number_of_cylinders=8                           //Number of cylinders
max_rated_rpm= 2150                             //Max rated RPM  2700
max_rated_hp= 575                               //Max rated HP  180
fuel_metering_type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 35.04                                //Max design manifold pressure, (inHg) 0
min_design_mp= 0                                //Min design manifold pressure, (inHg) 0
critical_altitude= 8856                            //Altitude to which the turbocharger will provide max design manifold pressure (feet) 0
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction

[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