[fltsim.0]
title=Mikoyan 1.44
sim=mig35
model=
panel=
sound=
texture=
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=01
atc_airline=AIRFORCE
atc_flight_number=
ui_manufacturer=Mikoyan
ui_type=Product 1.44
ui_variation=Blue 01
description=The Product 1.44 is the aerodynamic test prototype of the 1.42 (MiG-35) Russian fifth-generation fighter.
atc_heavy=0

[General]
atc_type=
atc_model=
performance=Maximum Speed\n2,600 km\/hr\n\nEngine\nTwo Lyulka-Saturn AL-41F turbofans rated at 185 kN\n\nMaximum Range\n4,000 km\n\nService Ceiling\n18.5 km\n\nMaximum Gross Weight\n34,500 kg        \n\nLength\n20.5 m (without probe)\n\nWingspan\n16.4 m\n\nHeight\n5.6 m\n\nMaximum Weapons Load\n6,500 kg

[WEIGHT_AND_BALANCE]
max_gross_weight=77162.000
empty_weight=36376.000
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
station_load.0=0.000000,0.000000,0.000000,0.000000
;Moments of Inertia
empty_weight_pitch_MOI=203000.000
empty_weight_roll_MOI=52300.000
empty_weight_yaw_MOI=168000.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000
max_number_of_stations=50

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.309
aileron_effectiveness=1.209
rudder_effectiveness=1.000
pitch_stability=0.800
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[jet_engine]
thrust_scalar=1.000

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
fuel_transfer_pump=0, 10, 17.0
flap_motor=0, 5, 17.0
gear_motor=0, 5, 17.0
autopilot=0, 5, 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5, 17.0
pitot_heat=0, 2, 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2, 17.0
gear_warning=0, 2, 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=float>
//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=1.000, 14.400, 0.000, -7.000, 1181.100, 0.000, 2.034, 50.000, 0.200, 2.500, 0.800, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1.000, -5.400, -5.900, -7.000, 1574.800, 1.000, 3.379, 0.000, 0.200, 2.500, 0.800, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -5.400, 5.900, -7.000, 1574.800, 2.000, 3.379, 0.000, 0.200, 2.500, 0.800, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -19.000, -26.000, 0.700, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4=2.000, -19.000, 26.000, 0.700, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5=2.000, -16.800, 10.500, -3.400, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6=2.000, -16.800, -10.500, -3.400, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
static_pitch=2.000
static_cg_height=7.000
gear_system_type=0

[Views]
eyepoint=22.5, 0.12, 4.4

[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1

[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.
elevator=150, 250
aileron=150, 250
rudder=150, 250

[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

[pitot_static]
vertical_speed_time_constant=99

[exits]
number_of_exits=1
exit_rate.0=0.4

[LIGHTS]
//lon, lat, vert
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1=2, 1.0, 0.0, 4.04, fx_beacon
light.2=2, -3.6, 0.0, -3.0, fx_strobe
light.3=3, -17,  26.8, 0.6, fx_navgre
light.4=3, -17, -26.8, 0.6, fx_navred

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[fuel]
LeftMain=0.000, -2.000, 0.000, 2000.000, 0.000
RightMain=0.000, 2.000, 0.000, 2000.000, 0.000
fuel_type=2.000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=1054.000
wing_span=51.840
wing_root_chord=28.120
wing_dihedral=0.000
wing_incidence=0.250
wing_twist=0.000
oswald_efficiency_factor=0.900
wing_winglets_flag=0
wing_sweep=54.000
wing_pos_apex_lon=-26.000
wing_pos_apex_vert=0.700
htail_area=86.560
htail_span=27.000
htail_pos_lon=10.400
htail_pos_vert=2.600
htail_incidence=0.000
htail_sweep=60.000
vtail_area=128.240
vtail_span=10.100
vtail_sweep=44.000
vtail_pos_lon=-21.100
vtail_pos_vert=11.100
elevator_area=86.560
aileron_area=19.240
rudder_area=30.780
elevator_up_limit=30.000
elevator_down_limit=30.000
aileron_up_limit=30.000
aileron_down_limit=30.000
rudder_limit=30.000
elevator_trim_limit=20.000
spoiler_limit=0.000
spoilerons_available=0
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=0.000

[GeneralEngineData]
engine_type=1
Engine.0=-8.300, 2.100, 0.000
Engine.1=-8.300, -2.100, 0.000
fuel_flow_scalar=1.000
//FS2004
min_throttle_limit=0.0   //Minimum percent throttle. Generally negative for turbine reverser

[brakes]
parking_brake=1        //Parking brake available
toe_brakes_scale=0.67  //Brake scalar

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000    //PSI

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1    //Turn AND Bank

[stall_warning]
type=1

[gear_warning_system]
gear_warning_available=1 //Normal
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=20.0 //Flap angle that activates warning at idle
flap_limit_power=30.0 //Flap angle that activates warning at above idle
//

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=8.000
rated_N2_rpm=29920.000
static_thrust=20780.000
afterburner_available=1
reverser_available=0

[Reference Speeds]
flaps_up_stall_speed=152.000
full_flaps_stall_speed=110.000
cruise_speed=700.000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8
//FS2004
default_pitch_mode=0
default_bank_mode=0
max_pitch=40.000
max_pitch_acceleration=1.000
max_pitch_velocity_lo_alt=2.000
max_pitch_velocity_hi_alt=1.500
max_pitch_velocity_lo_alt_breakpoint=20000.000
max_pitch_velocity_hi_alt_breakpoint=28000.000
max_bank=40.000
max_bank_acceleration=1.800
max_bank_velocity=3.000
max_throttle_rate=0.100
nav_proportional_control=9.000
nav_integrator_control=0.250
nav_derivative_control=0.000
nav_integrator_boundary=2.500
nav_derivative_boundary=0.000
gs_proportional_control=9.520
gs_integrator_control=0.260
gs_derivative_control=0.000
gs_integrator_boundary=0.700
gs_derivative_boundary=0.000
yaw_damper_gain=1.000

[forcefeedback]
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=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 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

[Flaps.0]
type=2
span-outboard=0.800
extending-time=3.000
system_type=1
damaging-speed=350.000
blowout-speed=300.000
lift_scalar=1.000
drag_scalar=1.300
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=10.000, 0.000

[Flaps.1]
type=1
span-outboard=0.400
extending-time=5.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=0.800
drag_scalar=1.500
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=20.000, 0.000
flaps-position.3=30.000, 0.000