[fltsim.0]
title=Yakovlev Yak-50 - DDR-Flugzeuge.de
sim=Yak50
model=
panel=
sound=
texture=DDR
kb_checklists=
description=Yakovlev Yak-50 \n(c) Ralf Kreibich 2004-2007 \n FDE: "FlusiRainer" Mehlin
ui_manufacturer=Yakovlev
ui_type=Yak-50
ui_variation=GST 1986
atc_heavy=0
atc_id=?????
atc_airline=GST
atc_flight_number=271064


[General]
atc_type=Yakovlev
atc_model=YK50
editable=1

[WEIGHT_AND_BALANCE]
empty_weight=			1686				// (pounds)
reference_datum_position=0.0000, 0.0000, 0.0000       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000

;Moments of Inertia
empty_weight_pitch_MOI=			3181.10
empty_weight_roll_MOI=			2396.69
empty_weight_yaw_MOI=			3475.84
empty_weight_coupled_MOI=0.000000
max_gross_weight=				1984.000000

[fuel]
Center1=				3.000000,0.000000,0.000000,25.00,0.000000
fuel_type=				1.000000
number_of_tank_selectors=	1
electric_pump=			1

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=2.0
aileron_effectiveness=1.5
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[piston_engine]
power_scalar=				1.0
cylinder_displacement=			76.6			//85.000000
compression_ratio=			5.900000
number_of_cylinders=			9
max_rated_rpm=				3500.000000
max_rated_hp=				269			//365.000000
fuel_metering_type=			0
cooling_type=				0
normalized_starter_torque=		0.75000
turbocharged=				0
max_design_mp=				40.0
min_design_mp=				1.000000
critical_altitude=			21653.000000
emergency_boost_type=			3
emergency_boost_mp_offset=		5.000000
emergency_boost_gain_offset=		0.480000
fuel_air_auto_mixture=			1
auto_ignition=				076.6		
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
thrust_scalar = 		1.0                             //Propeller thrust scalar
propeller_type= 		0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 	6.8                         //Propeller Diameter, (feet)
propeller_blades= 	2                             //Number of propeller blades
propeller_moi= 		20.0                             //Propeller moment of inertia
beta_max= 			65.0                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 			21.2                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 		1100.0                             //Miminum governed RPM
prop_tc= 			0.1                                    //Prop time-constant
gear_reduction_ratio= 	0.86                     //Propeller gear reduction ratio
fixed_pitch_beta= 0.0                           //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 1                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 1                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0                      //Minimum RPM for prop feathering
beta_feather= 82.5                              //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9                          //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available= 0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0                     //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0                       //Minimum pitch angle in reverse, (degrees)

[exits]
number_of_exits=1
exit_rate.0=0.4  				;Percent per second

[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0

[contact_points]
//0  Class
//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)

//point.0=1, -14.85,  0.00, -1.55, 1600, 0, 0.33, 85.0, 0.20, 1.0, 1.0, 	0.0, 0.0, 	0, 0, 300
//point.1=1,   2.90, -3.95, -5.26, 2200, 1, 1.00,  0.0, 0.50,1.50, 1.00, 	7.5, 7.5, 	2, 0, 200
//point.2=1,   2.90,  3.95, -5.26, 2200, 2, 1.00,  0.0, 0.50, 1.50, 1.00, 	6.0, 6.0, 	3, 0, 200

point.0=1, -14.702, 0.00, -1.47, 1600, 0, 0.66, 0.0, 0.2, 2.2, 0.6, 5.0, 5.0, 0.0, 135.0, 140.0

point.1=1,   3.40, -3.95, -5.55, 2200, 1, 0.82, 0.0, 0.3, 2.5, 0.7, 5.2, 4.8, 2.0, 135.0, 140.0
point.2=1,   3.40,  3.91, -5.55, 2200, 2, 0.82, 0.0, 0.3, 2.5, 0.7, 5.2, 4.8, 2.0, 135.0, 140.0


point.3=2,   0.00,-20.00, -1.25, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5
point.4=2,   0.00, 20.00, -1.25, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6
point.5=2, -16.25,  0.00,  0.00, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9
point.6=2,   6.41,  0.00, -1.70, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4

static_cg_height=		4.30           //feet, altitude of CG when at rest on the ground
static_pitch=3.6698         	//degrees (pitch when loaded on ground)
gear_system_type=		1

[brakes]
toe_brakes_scale=0.650000
parking_brake=1


[Views]
//eyepoint=-3.37,0.000000,1.979
eyepoint=-3.97,0.000000,1.679

[LIGHTS]
panel=0.00, 0.15, -0.80, fx_vclight

[airplane_geometry]
wing_area=177.000000
wing_span=31.160000
wing_root_chord=5.916667
wing_dihedral=4.998779
wing_incidence=0.0
wing_twist=0.000000
oswald_efficiency_factor=0.75
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=32.000000
htail_span=12.250000
htail_pos_lon=-16.416667
htail_pos_vert=0.000000
htail_incidence=0.0
htail_sweep=0.000000
vtail_area=29.000000
vtail_span=6.140033
vtail_sweep=0.000000
vtail_pos_lon=-17.916667
vtail_pos_vert=1.500000
elevator_area=12.820000
aileron_area=18.070000
rudder_area=8.230000
elevator_up_limit=30.00
elevator_down_limit=25.00
aileron_up_limit=16.999658
aileron_down_limit=16.999658
rudder_limit=30.00
elevator_trim_limit=19.996227
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[GeneralEngineData]
engine_type=0
Engine.0=7.500000,0.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[Reference Speeds]
flaps_up_stall_speed=102.000000
full_flaps_stall_speed=81.600000
cruise_speed=250.000000
max_indicated_speed=760.500000

[keyboard_response]
elevator=300.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[autopilot]
autopilot_available=0
flight_director_available=0
default_vertical_speed=700.000000
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

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks5
touchdown=fx_tchdwn_s5, 1

[hydraulic_system]
electric_pumps=		0
engine_map=			1,0,0,0
normal_pressure=		6.930556

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[direction_indicators]
direction_indicator.0=1,0


[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=75.000175,0.000000


[SMOKESYSTEM]
smoke.0=-0,-20.00,-4.00,fx_fallsw.fx