[fltsim.0]
title=AI-MiG29
sim=AI-MiG29v-2
model=w
texture=
atc_id=MiG 29 
ui_manufacturer=SBAI
ui_type=MiG-29
ui_variation=Test
description=MiG-29 "Fulcrum"
atc_parking_types=GATE
atc_parking_codes=MIL


[fltsim.1]
title=AI-MiG29-UB
sim=AI-MiG29v-2
model=UB_W
texture=UB
atc_id=MiG 29 
ui_manufacturer=SBAI
ui_type=MiG-29
ui_variation=Test
description=MiG-29 "Fulcrum"
atc_parking_types=GATE
atc_parking_codes=MIL



[General]
atc_type=MIG 
atc_model=MIG29 
performance=Length: 15.76 m (51'8 ft)\nWing span: 7.15 m (23'5 ft)\nWeight: 9800 kg (21600 lbs)\nPower:  6600 kg (14550 lbs) with Afterburner\nCeiling:  17000 m (56000 ft)\nRange: 1100 km (684 nm)\nSpeed: 1,146 kt (2.05 mach)\nDesign for FS2000: Kirk Olsson\nDesign for CFS2: Chris and Jim Coarse\nDate: 2001- 10-18\n\nHot Cargo Pad Upgrades\nhttp:\/\/flightsimmers.net\/airbase\/hotcargopad\n\n 
editable=0 

[weight_and_balance]

// ACM V2.3
max_gross_weight = 40969
empty_weight = 25110
reference_datum_position = -2.145, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 301732
empty_weight_roll_MOI = 46718
empty_weight_yaw_MOI = 202601
empty_weight_coupled_MOI = 0
max_number_of_stations = 1

station_load.0 = "0.0, 0.0,  0.0,	0.0, Load"	//9912


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -23, -6.25, 8.3, fx_navwhi
light.1 = 2, -21, -3, -1.0, fx_AIafterburner_TRDM29,
light.2 = 2, -21, 3, -1.0, fx_AIafterburner_TRDM29,
light.3 = 2, -21, -3, -1.0, fx_AIsmoke_TRD,
light.4 = 2, -21, 3, -1.0, fx_AIsmoke_TRD,
light.5 = 3, -11, -19.68, 0, fx_navred
light.6 = 3, -11, 19.68, 0, fx_navgre

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.0
engine.0 = -21, -3, -1.1,
engine.1 = -21, 3, -1.1,
min_throttle_limit=-0.250000

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown =  fx_AIT_M

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1

Center1 = 0, 0, 0, 1009, 0
electric_pump=0


[contact_points]
static_pitch = 0.5
static_cg_height = 6.4
tailwheel_lock = 0
max_number_of_points = 3

        //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,  6.76,  0, -6.45,  2200, 0, 0.9, 55, 0.3, 2.5, 0.9, 8, 8, 0, 250, 270
point.1 = 1, -5.67, -5, -6.6,   2500, 2, 1.4,  0, 0.5, 2.5, 0.55, 8, 8, 2, 250, 270
point.2 = 1, -5.67,  5, -6.6,   2500, 2, 1.4,  0, 0.5, 2.5, 0.55, 8, 8, 3, 250, 270
//point.0 = 1,  6.76,  0, -6.85,   2200, 0, 0.9, 55, 1,   0.9, 0.9, 8, 8, 0, 250, 270
//point.1 = 1, -5.67, -5, -7.1,   2500, 2, 1.4,  0, 1.2, 0.9, 0.9, 8, 8, 2, 250, 270
//point.2 = 1, -5.67,  5, -7.1,   2500, 2, 1.4,  0, 1.2, 0.9, 0.9, 8, 8, 3, 250, 270
gear_system_type=0


[keyboard_response]
elevator = 150.000000, 250.000000
aileron = 150.000000, 250.000000
rudder = 150.000000, 250.000000


[forcefeedback]

[airplane_geometry]
//ACM_AREAW1// 0,0,0,3.0174,0.7774,0.7774,0.7774,3.6442,1.5549,1.5549
//ACM_AREAW2// 1.5549,4.2708,2.3327,2.3327,2.3327,4.8976,3.1103,3.1103,3.1103,5.5243
//ACM_AREAW3// 3.8877,3.8877,3.8877,6.1510,4.6654,4.6654,4.6654,6.7775,5.4429,5.4429
//ACM_AREAW4// 5.4429,7.4043,6.2206,6.2206,6.2206,8.0311,6.9980,6.9980,6.9980,8.6576
//ACM_AREAH1// 0,0,0,1.7474,0.2912,0.2912,0.1358,1.7956,0.5824,0.5824
//ACM_AREAH2// 0.2716,1.8443,0.8737,0.8737,0.4074,1.8926,1.1648,1.1648,0.5432,1.9412
//ACM_AREAH3// 1.4562,1.4562,0.6790,1.9895,1.7474,1.7474,0.8148,2.0381,2.0387,2.0387
//ACM_AREAH4// 0.9506,2.0864,2.3299,2.3299,1.0865,2.1349,2.6212,2.6212,1.2223,2.1833
//ACM_AREAV1// 0,0,0,2.2555,0.2506,0.2506,0.1446,2.2197,0.5012,0.5012
//ACM_AREAV2// 0.2892,2.1840,0.7518,0.7518,0.4338,2.1482,1.0024,1.0024,0.5787,2.1124
//ACM_AREAV3// 1.2530,1.2530,0.7232,2.0766,1.5036,1.5036,0.8679,2.0408,1.7539,1.7539
//ACM_AREAV4// 1.0125,2.0051,2.0048,2.0048,1.1575,1.9694,2.2555,2.2555,1.3020,1.9335
//ACM_CAREAW1// 3.4990,3.4990,5.0078,5.6111,3.8877,3.8877,5.3965,5.9699,4.2765,4.2765
//ACM_CAREAW2// 5.7852,6.3284,4.6654,4.6654,6.1742,6.6872,5.0542,5.0542,6.5630,7.0458
//ACM_CAREAW3// 5.4429,5.4429,6.9517,7.4043,5.8316,5.8316,7.3404,7.7630,6.2206,6.2206
//ACM_CAREAW4// 7.7293,8.1216,6.6093,6.6093,8.1181,8.4799,6.9980,6.9980,8.5066,8.8388
//ACM_CAREAH1// 0,0,0.8737,1.7474,0.2912,0.2912,1.0095,1.8394,0.5824,0.5824
//ACM_CAREAH2// 1.1453,1.9313,0.8737,0.8737,1.2812,2.0236,1.1648,1.1648,1.4170,2.1159
//ACM_CAREAH3// 1.4562,1.4562,1.5528,2.2081,1.7474,1.7474,1.6885,2.3001,2.0387,2.0387
//ACM_CAREAH4// 1.8243,2.3921,2.3299,2.3299,1.9601,2.4844,2.6212,2.6212,2.0959,2.5766
//ACM_CAREAV1// 0,0,0.5637,1.6914,0.2506,0.2506,0.7085,1.7460,0.5012,0.5012
//ACM_CAREAV2// 0.8532,1.8005,0.7518,0.7518,0.9979,1.8550,1.0024,1.0024,1.1426,1.9095
//ACM_CAREAV3// 1.2530,1.2530,1.2869,1.9637,1.5036,1.5036,1.4320,2.0183,1.7539,1.7539
//ACM_CAREAV4// 1.5765,2.0729,2.0048,2.0048,1.7214,2.1273,2.2555,2.2555,1.8660,2.1816
wing_area = 409.14
wing_span = 37.25
wing_root_chord = 21.3
wing_dihedral = -3
wing_incidence = 0.5
wing_twist = 0.0
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 42
wing_pos_apex_lon = 7.32
wing_pos_apex_vert = 1
htail_area = 67.0
htail_span = 27
htail_pos_lon = -8.5
htail_pos_vert = 0
htail_incidence = 0
htail_sweep = 48
vtail_area = 42.0
vtail_span = 9
vtail_sweep = 48
vtail_pos_lon = -11
vtail_pos_vert = 1
elevator_area = 17.0
aileron_area = 13.5
rudder_area = 7.3
elevator_up_limit = 20.0
elevator_down_limit = 6.0
aileron_up_limit = 5.0
aileron_down_limit = 5.0
rudder_limit = 24.0
elevator_trim_limit = 15.0
spoiler_limit = 60.0
aileron_to_spoileron_gain = 2.0
min_ailerons_for_spoilerons = 5
min_flaps_for_spoilerons = 4
spoilerons_available = 1

[electrical]
max_battery_voltage = 12
generator_alternator_voltage = 13
max_generator_alternator_amps = 40
electric_always_available = 0
avionics_bus = 0, 5, 9.5
avionics = 1, 5, 9.5
additional_system = 0, 2, 9.5
marker_beacon = 1, 2, 9
fuel_pump = 0, 5, 9

[flight_tuning]
cruise_lift_scalar=0.75 //1.0
parasite_drag_scalar=1.0 
induced_drag_scalar=1.5 //1.0
elevator_effectiveness=2.0 //1.0
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
pitch_stability=1.0 //1.25
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=0.25 //0.5
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=0.5 //1.0

[TurbineEngineData]
fuel_flow_gain=0.0025  //Gain on fuel flow
inlet_area=5.24   //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920  //RPM, second stage compressor rated value
static_thrust=24818  //Lbs, max rated static thrust at Sea Level: fors-8300, max-5040
afterburner_available=1  //Afterburner available?
reverser_available=1  //Thrust reverser available?

[jet_engine]
thrust_scalar=1.0 

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    = 15.0     //Flap angle that activates warning at idle
flap_limit_power   = 30.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.0	//0.5  //Brake scalar

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint=0.0, 0.0, 0.0 

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.6	                                // 0.0 .. 1.0
extending-time   = 15	                                // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 10		                        // degrees
flaps-position.2 = 20                                   // degrees
flaps-position.3 = 30                                   // degrees
flaps-position.4 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar= 2.5	//1.0
drag_scalar= 0.75	//1.0
pitch_scalar= 0.251.0

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1, 0 
Com.2=1, 0 
Nav.1=1, 0, 1 
Nav.2=1, 0, 0 
Adf.1=1 
Transponder.1=1 
Marker.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 = 2
attitude_indicator.1 = 1 

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

[Reference Speeds]
flaps_up_stall_speed=124.0		//Knots True (KTAS)
full_flaps_stall_speed=106.0 		//Knots True (KTAS)
cruise_speed=811                	//Knots True (KTAS)
max_mach                = 2.3
max_indicated_speed     = 1324          //Red line (KIAS)

[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=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
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

[stall_warning]
type=2