[fltsim.0]
title=Mil Mi-1
sim=Mi-1
model=
panel=
sound=
texture=
prop_anim_ratio=-1.30
atc_id_color=
atc_id=CCCP-010
ui_manufacturer=Mil
ui_type=Mi-1
ui_variation="AEROFLOT"
description="Russian helicopters Mil Mi-4. "




[General]
atc_type=Mil
atc_model=Mi-4
performance=Cruise Speed  80 kts\Maximum speed: 185 km/h (116 mph)\Powerplant: 1 Ч Shvetsov ASh-82V radial engine, 1,250 kW (1,675 hp)\Service ceiling: 5,500 m (18,040 ft)\nRate of Climb 600'per min\nFuel Capacity  Internal 185 U.S. gal\Range: 500 km (313 mi)\Empty weight: 5,100 kg (11,220 lb)\Max. takeoff weight: 7,550 kg (16,610 lb)\nSeating 2 Crew & 8-12 Passengers
editable=1 
Category=helicopter

[WEIGHT_AND_BALANCE]
max_gross_weight 	= 14940   
empty_weight 	= 5950    
reference_datum_position =  0.33,  0.0, 0.0   
empty_weight_CG_position = -0.73,  0.0, 0.0   

max_number_of_stations = 8
station_load.0 = "210, 2.6,  2.20, 0.0, Pilot"       
station_load.1 = "210, 2.6, -2.20, 0.0, Passenger"      

;Moments of Inertia
empty_weight_pitch_MOI   = 21000
empty_weight_roll_MOI    = 23000
empty_weight_yaw_MOI     = 29000
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
autopilot          = 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

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 
light.0 =  3,  21.50,  -5.90,  -1.55,  fx_navred ,
light.1 = 3,  21.50,   2.50,  -1.55,   fx_navgre ,
light.2 =  3, -25.75, -1.80,  2.50,  fx_navwhi ,
light.3 = 1,  4.71,  -1.80,  -5.70,    fx_beacon ,
light.4 = 4,  11.71,  -1.80,  4.50, fx_strobe ,
light.5 = 5,  24.07,  0.45, -5.10,  fx_landing ,
light.6 = 5,  24.07,  -0.01, -5.10,  fx_landing ,




[TailHook]
tailhook_length=5				;(feet)
tailhook_position=-8.35, 0.0, -1.0  ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0

[contact_points]
static_pitch = 3.8
static_cg_height = 7.9
gear_system_type = 1
max_number_of_points = 3

point.0 = 1,   9.86,   0.00, -10.50, 8200, 0, 0.98, 60, 0.32, 1.5, 0.75, 3.5, 3.5, 0, 150, 150
point.1 = 1,  -3.92,  -6.90, -10.00, 8200, 1, 1.44,  0, 0.56, 0.8, 0.85, 3.5, 3.5, 2, 150, 150
point.2 = 1,  -3.92,   6.90, -10.00, 8200, 2, 1.44,  0, 0.56, 0.8, 0.85, 3.5, 3.5, 3, 150, 150

[Views]
eyepoint= 2.4, 1.4, 7.0 

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


[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=0,0

[Reference Speeds]
cruise_speed            = 80    
max_indicated_speed     = 115   

[autopilot]
autopilot_available= 0
flight_director_available= 0

[yaw_string]
yaw_string_available=1

[brakes]
parking_brake = 1       	
toe_brakes_scale = 1.0  	   

[hydraulic_system]
normal_pressure = 0.0    	 

[pitot_static]
pitot_heat=1.000000

[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=5.150000
engine_map=1,0,0,0

[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000

[deice_system]
structural_deice_type=2

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

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
Center1 =   0.0, 0,  -5, 112, 6
Center2 =  -1.0, 0,  -5,  83, 4
electric_pump=0

[GeneralEngineData]
engine_type = 0                              
Engine.0 = -0.5, 0.0, 0.0                      
fuel_flow_scalar= 1.0                        
min_throttle_limit =  0.0;                     

[piston_engine]
power_scalar = 1.0                             
cylinder_displacement= 90.0                   
compression_ratio= 8.5                         
number_of_cylinders=9                      
max_rated_rpm= 2700                            
max_rated_hp= 700                             
fuel_metering_type= 1                       
cooling_type= 0                                
normalized_starter_torque= 0.3               
turbocharged= 0                              
max_design_mp= 0                              
min_design_mp= 0                            
critical_altitude= 0                         
emergency_boost_type= 0                   
emergency_boost_mp_offset= 0                  
emergency_boost_gain_offset= 0                
fuel_air_auto_mixture= 0                       
auto_ignition= 0                            
max_rpm_mechanical_efficiency_scalar= 1.0      
idle_rpm_mechanical_efficiency_scalar= 1.0     
idle_rpm_friction_scalar= 1.0                   
max_rpm_friction_scalar=1.000000

[Helicopter]
reference_length       			=  21.69  
reference_frontal_area 			=  17.9
reference_side_area    			=  44.5
side_aero_center      			= -11.5
right_trim_scalar      			=   1.0
correlator_available   			=   1
governed_pct_rpm_ref  	      	=   1.0
governor_pid 				=   0.4, 0, 0.1, 0, 0.2
rotor_brake_scalar     			=   2.5
torque_scalar          			=   3.0
cyclic_roll_control_scalar 		=   1.7
cyclic_pitch_control_scalar 		=   0.8
pedal_control_scalar        		=   1.3
collective_on_rotor_torque_scalar 	=   1.0

[fuselage_aerodynamics]
drag_force_cf      = 4.45
side_drag_force_cf = 11.0
pitch_damp_cf      = -5.1
roll_damp_cf       = -5.1
yaw_damp_cf        = -3.2
yaw_stability_cf   =  0.28

[MainRotor]
Position 			= -0.5, 0.0, 4.91      
Radius   			= 12.683                 
max_disc_angle 		= 5.0
RatedRpm 			= 510
Number_of_blades 		= 2
Weight_per_blade 		= 27.0
Weight_to_moi_factor 	= 0.59
inflow_vel_reference 	= 57.0

[SecondaryRotor]
Position 		= -27.6, -0.84, 1.9       
TailRotor 		= 1					
Radius   		= 2.45