[fltsim.0]
title=Mig29A
sim=Mig29
model=1
panel=
sound=
texture=
kb_checklists=Mig29_check
kb_reference=Mig29_ref
description=The Mikoyan MiG-29 (NATO reporting name Fulcrum) is a fighter aircraft designed for the air superiority role in the Soviet Union. Developed in the 1970s by the Mikoyan design bureau, it entered service in 1983 and remains in use by the Russian Air Force as well as in many other nations.
ui_manufacturer=Mikoyan
ui_type=Mig29A
ui_variation=Poland
ui_typerole="Military Aircraft"
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.1]
title=Mig29A armed
sim=Mig29
model=
panel=
sound=
texture=
kb_checklists=Mig29_check
kb_reference=Mig29_ref
description=The Mikoyan MiG-29 (NATO reporting name Fulcrum) is a fighter aircraft designed for the air superiority role in the Soviet Union. Developed in the 1970s by the Mikoyan design bureau, it entered service in 1983 and remains in use by the Russian Air Force as well as in many other nations.
ui_manufacturer=Mikoyan
ui_type=Mig29A
ui_variation=Poland armed
ui_typerole="Military Aircraft"
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.2]
title=Mig29A Paint1
sim=Mig29
model=1
panel=
sound=
texture=1
kb_checklists=Mig29_check
kb_reference=Mig29_ref
description=The Mikoyan MiG-29 (NATO reporting name Fulcrum) is a fighter aircraft designed for the air superiority role in the Soviet Union. Developed in the 1970s by the Mikoyan design bureau, it entered service in 1983 and remains in use by the Russian Air Force as well as in many other nations.
ui_manufacturer=Mikoyan
ui_type=Mig29A
ui_variation=USSR
ui_typerole="Military Aircraft"
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.3]
title=Mig29A armed Paint1
sim=Mig29
model=
panel=
sound=
texture=1
kb_checklists=Mig29_check
kb_reference=Mig29_ref
description=The Mikoyan MiG-29 (NATO reporting name Fulcrum) is a fighter aircraft designed for the air superiority role in the Soviet Union. Developed in the 1970s by the Mikoyan design bureau, it entered service in 1983 and remains in use by the Russian Air Force as well as in many other nations.
ui_manufacturer=Mikoyan
ui_type=Mig29A
ui_variation=USSR armed
ui_typerole="Military Aircraft"
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.4]
title=Mig29A Paint2
sim=Mig29
model=1
panel=
sound=
texture=2
kb_checklists=Mig29_check
kb_reference=Mig29_ref
description=The Mikoyan MiG-29 (NATO reporting name Fulcrum) is a fighter aircraft designed for the air superiority role in the Soviet Union. Developed in the 1970s by the Mikoyan design bureau, it entered service in 1983 and remains in use by the Russian Air Force as well as in many other nations.
ui_manufacturer=Mikoyan
ui_type=Mig29A
ui_variation=Germany
ui_typerole="Military Aircraft"
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.5]
title=Mig29A armed Paint2
sim=Mig29
model=
panel=
sound=
texture=2
kb_checklists=Mig29_check
kb_reference=Mig29_ref
description=The Mikoyan MiG-29 (NATO reporting name Fulcrum) is a fighter aircraft designed for the air superiority role in the Soviet Union. Developed in the 1970s by the Mikoyan design bureau, it entered service in 1983 and remains in use by the Russian Air Force as well as in many other nations.
ui_manufacturer=Mikoyan
ui_type=Mig29A
ui_variation=Germany armed
ui_typerole="Military Aircraft"
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=



[General]
Performance=Length: 17.37 m (57 ft) ,Wingspan: 11.4 m (37 ft 3 in) ,Height: 4.73 m (15 ft 6 in) ,Wing area: 38 m? (409 ft?) ,Empty weight: 11,000 kg (24,250 lb) ,Loaded weight: 16,800 kg (37,000 lb) ,Max takeoff weight: 21,000 kg (46,300 lb) ,Powerplant: 2? Klimov RD-33K afterburning turbofans, 86.4 kN (20,725 lbf) each -Performance-Maximum speed: 2,445 km\/h (1,518 mph) ,Range: 700 km combat, 2,900 km ferry (430 mi \/ 1,800 mi) ,Service ceiling: 18,013 m \/ 59 060 ft (59,100 ft) ,Rate of climb: 330 m\/s (65,000 ft\/min) ,Wing loading: 442 kg\/m? (90.5 lb\/ft?) ,Thrust\/weight: 1.05
atc_type=Mikoyan 
atc_model=MiG29 
editable=1
Category = airplane

[CameraDefinition.0]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 0.5, -25.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 15, 1.0, 3.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -15, 1.0, 3.0
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.001]
Title = "Engine Controls"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.0, 0.25, -0.2
InitialPbh=48, 0, 27 

[Flight_tuning]
elevator_effectiveness=1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
pitch_stability=1.0 
roll_stability=1.0 
yaw_stability=1.0 
cruise_lift_scalar=1.0 
hi_alpha_on_roll= 1.0
hi_alpha_on_yaw=1.0
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 

[weight_and_balance]

max_gross_weight = 37000.000
empty_weight = 24250.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = -5.453, 0.000, -2.70
empty_weight_pitch_MOI   = 176600
empty_weight_roll_MOI    = 50500
empty_weight_yaw_MOI     = 154300
empty_weight_coupled_MOI = 0.0
max_number_of_stations = 2

station_load.0 =170.000000, 8.000000, 0.000000, 2.200000, Pilot
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=Taxi, 7=recognition,
//8 = wing,  9 = Logo, 10 = Cabin



light.0  = 3,  -12.10,  -18.3,  -2.00,  fx_navredm ,
light.1  = 3,  -12.10,   18.3,  -2.00,  fx_navgrem ,
light.2  = 3,  -24.70,  -6.40,   4.80,  fx_navwhi ,
light.3  = 3,  -24.70,   6.40,   4.80,  fx_navwhi
light.4  = 1,  -12.00,   2.60,  -5.20,  fx_beaconb ,
light.5  = 2,  -12.00,   2.60,  -5.20,  fx_strobe ,
light.6  = 1,  -12.00,  -2.60,  -5.20,  fx_beaconb ,
light.7  = 2,  -12.00,  -2.60,  -5.20,  fx_strobe ,
light.8  = 1,  -22.00,  -6.40,   7.30,  fx_beaconh ,
light.9  = 1,  -22.00,   6.60,   7.30,  fx_beaconh,
light.10 = 4,    9.50,   0.00,   2.50,  fx_vclight,
light.11 = 9,  -23.00,  -2.6,   -3.52,  fx_afterburner, 
light.12 = 9,  -23.00,   2.6,   -3.52,  fx_afterburner, 

[GeneralEngineData]

engine_type = 1
engine.0 = -24.500, -2.8, -3.5
engine.1 = -24.500,  2.8, -3.5
fuel_flow_scalar = 1.000
min_throttle_limit=-0.15

[Jet_engine]
thrust_scalar=1.0 

[TurbineEngineData]
fuel_flow_gain= 0.006 
inlet_area= 7.000 
rated_N2_rpm= 16000
static_thrust= 12900.000
afterburner_available   = 6                     
afterburner_throttle_threshold = 0.95          
reverser_available      = 1                     
ThrustSpecificFuelConsumption = 1.0             
AfterBurnThrustSpecificFuelConsumption = 1.3   


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
touchdown=fx_tiremark_8, 1
startup=fx_AB_StartupSmoke.fx

 
[fuel]
fuel_type = 2
number_of_tank_selectors =1
Center1 = -5.083, 0.000, -1.250, 1536.000, 0.000
electric_pump=1


[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


point.0 = 1,   6.50,   0.00, -8.30, 2000.0, 0.0, 0.70, 25.0, 0.60, 2.50, 0.70, 5.00, 5.00, 0.00, 0.00, 0.00
point.1 = 1,  -7.50,  -6.50, -8.10, 2000.0, 1.0, 1.15,  0.0, 0.60, 2.50, 0.70, 5.00, 5.00, 2.00, 0.00, 0.00
point.2 = 1,  -7.50,   6.50, -8.10, 2000.0, 2.0, 1.15,  0.0, 0.60, 2.50, 0.70, 5.00, 5.00, 3.00, 0.00, 0.00
point.3 = 2, -12.60, -16.10, -1.30, 1574.0, 0.0, 0.00,  0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00
point.4 = 2, -12.60,  16.10, -1.30, 1574.0, 0.0, 0.00,  0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00
point.5 = 2, -16.47,   0.00, -2.70, 1574.0, 0.0, 0.00,  0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00
point.6 = 2,   9.82,   0.00, -2.60, 1574.0, 0.0, 0.00,  0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
gear_system_type=3

static_pitch= 0.000
static_cg_height= 7.800
gear_system_type=1           //Hydraulic

[keyboard_response]
elevator = 500.0, 900.0
aileron = 500.0, 900.0
rudder = 500.0, 900.0


[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

[airplane_geometry]
wing_area = 412
wing_span = 37.3
wing_root_chord = 18.3
wing_dihedral = -3.00
wing_incidence = 2.00
wing_twist = 0.000
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 42.00
wing_pos_apex_lon = -5.0
wing_pos_apex_vert = -2.0
htail_area = 75.6
htail_span = 25.5
htail_pos_lon = -21.2
htail_pos_vert = -2.0
htail_incidence = 0.00
htail_sweep = 50.00
vtail_area = 104.5
vtail_span = 9.20
vtail_sweep = 47.501
vtail_pos_lon = -19.1
vtail_pos_vert = 4.0
elevator_area = 75.6
aileron_area = 10.2
rudder_area = 20.0
elevator_up_limit = 20.000
elevator_down_limit = 18.000
aileron_up_limit = 15.000
aileron_down_limit = 13.000
rudder_limit = 25.000
elevator_trim_limit = 8.000
spoiler_limit = 70.000
aileron_to_spoileron_gain = 0.00
min_ailerons_for_spoilerons = 0.00
min_flaps_for_spoilerons = 0.00
spoilerons_available = 0
auto_spoiler_available=0
spoiler_extension_time=2.60
positive_g_limit_flaps_up=4.0
positive_g_limit_flaps_down=4.0
negative_g_limit_flaps_up=-4.1
negative_g_limit_flaps_down=-4.1

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 100
electric_always_available = 0
autopilot = 0, 5, 22
avionics_bus = 0, 10, 22
avionics = 1, 5, 23
pitot_heat = 0, 2, 22
additional_system = 0, 14, 23
marker_beacon = 1, 2, 22
gear_warning = 0, 2, 22
fuel_pump = 0, 5, 22
starter1 = 0, 10, 22
starter2 = 0, 10, 22
light_nav = 0, 5, 22
light_beacon = 0, 2, 22
light_landing = 0, 2, 22
light_taxi = 0, 2, 22
light_strobe = 0, 2, 22
light_panel = 0, 5, 22
light_logo = 0, 5, 22
light_recognition = 0, 5, 22
standby_vacuum = 0, 5, 17
hydraulic_pump = 0, 5, 22
fuel_transfer_pump = 0, 5, 17

[Brakes]
parking_brake   = 1
toe_brakes_scale= 1.8

[Views]
eyepoint=9.0,0,2.14

[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
Transponder.1 = 1
Marker.1      = 1

[Hydraulic_system]
electric_pumps = 1
engine_map     = 1,1,0,0
normal_pressure= 4000.0

[Exits]
number_of_exits= 1
exit_rate.0    = 0.4

[LSO]
LSOAdjustSpeed= 1.05

[Gear_warning_system]
gear_warning_available= 0
pct_throttle_limit    = 5.0
flap_limit_power      = 29.0
flap_limit_idle       = 29.0

[Stall_warning]
type= 0
stick_shaker=1

[altimeters]
altimeter.0 = 1

[airspeed_indicators]
airspeed_indicator.0=1


[Direction_indicators]
direction_indicator.0=3,0 

[Attitude_indicators]
attitude_indicator.0= 1

[Turn_indicators]
turn_indicator.0= 1,0

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 1800.0
autothrottle_available= 0
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=45.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=18.52
gs_integrator_control=0.56
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
pitch_takeoff_ga=8.000000

[Reference Speeds]
full_flaps_stall_speed= 115.000 
flaps_up_stall_speed  = 129.000 
cruise_speed= 900.000 
max_indicated_speed   = 1600.0
max_mach              =    3.4

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 3.000
system_type= 0
lift_scalar= 1.60
drag_scalar= 1.400
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 35.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
lift_scalar= 1.60
drag_scalar= 1.400
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000

[pitot_static]
pitot_heat=1.000000

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[deice_system]
structural_deice_type=0