[fltsim.0]
title=Yak-41
sim=Yak141
model=
panel=
sound=
texture=
kb_checklists=
atc_id=41
atc_flight_number=41
ui_manufacturer=Yakovlev
ui_type=Yak-41
ui_variation=
ui_typerole="Military"
ui_createdby="haditahir"
description=
[general]
atc_type=Yakovlev
atc_model=Yak-41
performance="Take-off\t19 500 kg\n
Power plant:\n
cruise-lift engine\t15 500 kg\n
lift engine\n2 x 4 100 kg\n
Max. Speed\t1 800 km/h\n
Ceiling\t15 000 m\n
Range\t2 100 km"
category = airplane
[pitot_static]
vertical_speed_time_constant = 99
pitot_heat=1
[WEIGHT_AND_BALANCE]
reference_datum_position=0.0,0.0,0.0
empty_weight_CG_position=0.0,0.0,0.0
max_number_of_stations=50
station_load.0=0.0,0.0,0.0,0.0
empty_weight=25680.0
empty_weight_roll_MOI=14763.29
empty_weight_pitch_MOI=114133.33
empty_weight_yaw_MOI=71784.05
empty_weight_coupled_MOI=0.0
max_gross_weight=43000.0
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.0
aileron_effectiveness=1.00
rudder_effectiveness=1.000
pitch_stability=0.800
roll_stability=1.000
yaw_stability=1.0
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.200
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type=1
Engine.0= 12.2065, 0.000, 2.0095
fuel_flow_scalar=0.100000
min_throttle_limit=0.000000
[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=17.646
rated_N2_rpm=29920.000000
static_thrust=26550.600000
afterburner_available=1
reverser_available=0
afterburner_throttle_threshold = 0.76
[jet_engine]
thrust_scalar =1
[electrical]
max_battery_voltage=12.0
generator_alternator_voltage=13.8
max_generator_alternator_amps=40.0
avionics_bus=0, 10, 9.5
avionics=1, 5 , 9.5
additional_system=0, 20, 9.5
marker_beacon=1, 2 , 9.0
fuel_pump=0, 5 , 9.0
[contact_points]
// radius ban belakang 0,261m dpn 0,194m. satuannya ft
static_pitch=0
static_cg_height=5.6
gear_system_type=1
point.0=1, 15.833, 0,-5.5691, 1574.803150, 0, 0.7877, 60, 0.8897, 2.50,0.929877,5,5,0,0,0
point.1=1, -9, 4.917,-5.5580, 1574.803150, 1, 1.0674, 0.00, 0.6728, 2.50,0.902664,5,5,2,0,0
point.2=1, -9,-4.917,-5.5580, 1574.803150, 2, 1.0674, 0.00, 0.6728, 2.50,0.902664,5,5,3,0,0
point.3=2, -16.083,-16.33, 2.5923, 1574.803150, 0, 0.000000, 0.00, 0, 0,0,0,0,5,0,0 //-- L Wingtip
point.4=2, -16.083, 16.33, 2.5923, 1574.803150, 0, 0.000000, 0.00, 0, 0,0,0,0,6,0,0 //-- R Wingtip
point.5=2, -29.333, 3.917, 11.416, 1574.803150, 0, 0.000000, 0.00, 0, 0,0,0,0,9,0,0 //-- Tailtop
point.6=2, -27.50, 0, 2.6731, 1574.803150, 0, 0.000000, 0.00, 0, 0,0,0,0,4,0,0 //-- Tail
point.7=2, 28.0297, 0, 0.0280, 1574.803150, 0, 0.000000, 0.00, 0, 0,0,0,0,7,0,0 //-- Nose
// y , x, z
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.0
flap_limit_power=0.0
flap_limit_idle=0.0
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.1,0.1 ;Percent per second
[brakes]
toe_brakes_scale=1.000031
parking_brake=1
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2,3,4
[Views]
//kaki y,x,z
eyepoint=15.1218,0.0,4.3138
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=2.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=12.500000,0.000000
flaps-position.2=20.000000,0.000000
flaps-position.3=30.500000,0.000000
flaps-position.4=40.000000,0.000000
flaps-position.5=62.000000,0.000000
flaps-position.6=70.000000,0.000000
flaps-position.7=90.000000,0.000000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//6=taxi light, 7=recognition light, 8=wing light, 9=logo light
light.0=3, 21.336, 1.637, 0.455, fx_navwhi ,
light.1=3, 21.336, -1.637, 0.455, fx_navwhi ,
light.2= 4, 16, 0.00, 4.8, fx_vclight,
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Adf.2 = 1
Transponder.1 = 1
Marker.1 = 1
[keyboard_response]
elevator=150.0,250.0
aileron=150.0,250.0
rudder=150.0,250.0
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[altimeters]
altimeter.0=1
altimeter.1=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn AND Bank
[vacuum_system]
max_pressure=5.15 //PSI
vacuum_type=2 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1
[pneumatic_system]
max_pressure=18.000
bleed_air_scalar=1.000000
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=30,15
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[fuel]
LeftMain= -10.0, 6.5, 3.25, 500.0, 0.0
RightMain=-10.0, -6.5, 3.25, 500.0, 0.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=682.000000
wing_span=45.833
wing_root_chord=19.666667
wing_dihedral=9.036255
wing_incidence=-0.494
wing_twist=1.000
oswald_efficiency_factor=1.501108
wing_winglets_flag=0
wing_sweep=40.000000
wing_pos_apex_lon=-1.500000
wing_pos_apex_vert=3.500000
htail_area=280.000000
htail_span=18.666667
htail_pos_lon=-20.833333
htail_pos_vert=1.700000
htail_incidence=0.000000
htail_sweep=50.000000
vtail_area=100.000000
vtail_span=11.401754
vtail_sweep=50.000000
vtail_pos_lon=-21.333333
vtail_pos_vert=8.000000
elevator_area=109
aileron_area=64
rudder_area=46
elevator_up_limit=25
elevator_down_limit=25
aileron_up_limit=25
aileron_down_limit=25
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=45.000000
auto_spoiler_available=1
spoilerons_available=1
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
positive_g_limit_flaps_up=9.615385
positive_g_limit_flaps_down=9.615385
negative_g_limit_flaps_up=-9.615385
negative_g_limit_flaps_down=-9.615385
spoiler_extension_time=5.000000
[Reference Speeds]
flaps_up_stall_speed=500
//full_flaps_stall_speed=110.000
full_flaps_stall_speed=500.000
cruise_speed=966.000
max_indicated_speed=1587.000
max_mach=1.700
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
[stall_warning]
type=1
stick_shaker=0
[deice_system]
structural_deice_type=0
[CameraDefinition.0]
Title = "Tail"
Guid = {91840533-3C8D-41ac-ABEA-53B1A8EDADE7}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 1.5, -15.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum