//ALPHA FS9 MiG-25 Foxbat 2:30 PM 2/25/2004

[fltsim.0]
title=ALPHA MiG-25 Foxbat
sim=MiG-25 Foxbat
model=
panel=
sound=
texture=
kb_checklists=MiG-25 Foxbat_check
kb_reference=MiG-25 Foxbat_ref
ui_manufacturer=ALPHA
ui_type=MiG-25 Foxbat
ui_variation=1. Soviet AF, 4 x AA-6
description=© ALPHA Simulations 2004\n\nMiG-25 Foxbat\n\nDeveloped to counter the Lockheed A-12, the MiG-25 Foxbat is capable of 1,864 m.p.h. at optimum altitude. The first prototype first flew in 1964 and series production commenced in 1969. The type is still in service in several of the once Soviet-aligned states, such as Libya, Syria, Algeria and India.
atc_id_color=0000000000
visual_damage=0
atc_heavy=0
atc_id=MIG25
atc_airline=
atc_flight_number=

[fltsim.1]
title=ALPHA MiG-25 Foxbat clean
sim=MiG-25 Foxbat
model=clean
panel=
sound=
texture=
kb_checklists=MiG-25 Foxbat_check
kb_reference=MiG-25 Foxbat_ref
ui_manufacturer=ALPHA
ui_type=MiG-25 Foxbat
ui_variation=2. Soviet AF, clean configuration
description=© ALPHA Simulations 2004\n\nMiG-25 Foxbat\n\nDeveloped to counter the Lockheed A-12, the MiG-25 Foxbat is capable of 1,864 m.p.h. at optimum altitude. The first prototype first flew in 1964 and series production commenced in 1969. The type is still in service in several of the once Soviet-aligned states, such as Libya, Syria, Algeria and India.
atc_id_color=0000000000
visual_damage=0
atc_heavy=0
atc_id=MIG25
atc_airline=
atc_flight_number=

[fltsim.2]
title=ALPHA MiG-25 Foxbat camo
sim=MiG-25 Foxbat
model=
panel=
sound=
texture=white37
kb_checklists=MiG-25 Foxbat_check
kb_reference=MiG-25 Foxbat_ref
ui_manufacturer=ALPHA
ui_type=MiG-25 Foxbat
ui_variation=3. Soviet AF, camo, 4 x AA-6
description=© ALPHA Simulations 2004\n\nMiG-25 Foxbat\n\nDeveloped to counter the Lockheed A-12, the MiG-25 Foxbat is capable of 1,864 m.p.h. at optimum altitude. The first prototype first flew in 1964 and series production commenced in 1969. The type is still in service in several of the once Soviet-aligned states, such as Libya, Syria, Algeria and India.
atc_id_color=0000000000
visual_damage=0
atc_heavy=0
atc_id=MIG25
atc_airline=
atc_flight_number=

[fltsim.3]
title=ALPHA MiG-25 Foxbat clean camo
sim=MiG-25 Foxbat
model=clean
panel=
sound=
texture=white37
kb_checklists=MiG-25 Foxbat_check
kb_reference=MiG-25 Foxbat_ref
ui_manufacturer=ALPHA
ui_type=MiG-25 Foxbat
ui_variation=4. Soviet AF, camo, clean configuration
description=© ALPHA Simulations 2004\n\nMiG-25 Foxbat\n\nDeveloped to counter the Lockheed A-12, the MiG-25 Foxbat is capable of 1,864 m.p.h. at optimum altitude. The first prototype first flew in 1964 and series production commenced in 1969. The type is still in service in several of the once Soviet-aligned states, such as Libya, Syria, Algeria and India.
atc_id_color=0000000000
visual_damage=0
atc_heavy=0
atc_id=MIG25
atc_airline=
atc_flight_number=

[fltsim.4]
title=ALPHA MiG-25 Foxbat 2-str
sim=MiG-25 Foxbat
model=2str
panel=
sound=
texture=2s
kb_checklists=MiG-25 Foxbat_check
kb_reference=MiG-25 Foxbat_ref
ui_manufacturer=ALPHA
ui_type=MiG-25 Foxbat
ui_variation=5. Soviet AF, 2-seater
description=© ALPHA Simulations 2004\n\nMiG-25U Foxbat\n\nDeveloped to counter the Lockheed A-12, the MiG-25 Foxbat is capable of 1,864 m.p.h. at optimum altitude. The first prototype first flew in 1964 and series production commenced in 1969. The type is still in service in several of the once Soviet-aligned states, such as Libya, Syria, Algeria and India.
atc_id_color=0000000000
visual_damage=0
atc_heavy=0
atc_id=MIG25
atc_airline=
atc_flight_number=



[General]
performance=Model: P McDonell, P Perrott\nPanel: P Perrott\nTextures: P McDonell, P Perrott, D Swart\nFlight Model: J McDaniel\n\nLength: 78 ft 1.75 in\nWingspan: 45 feet 11.71 in\nWing area: 660 sq ft\nEmpty weight: 59,350 lbs\nMaximum weight: 90,586 lbs\nTop speed: Mach 2.82 at 43,650 ft\nPower: 2x Soyuz R-15BD-300, 19400 lbs st. thr.\nArmament: Up to 4,000 kg of missiles mounted on underwing hardpoints, generally comprising 4 long or short range air-to-air missiles for interception. 
editable=1 
atc_type= 
atc_model= 

[weight_and_balance]

// ACM V2.3
max_gross_weight = 90586
empty_weight = 59350
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 380096
empty_weight_roll_MOI = 67199
empty_weight_yaw_MOI = 268483
empty_weight_coupled_MOI = 0
max_number_of_stations =50

station_load.0 =0.000000,0.000000,0.000000,0.000000


[lights]

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

light.0 = 2, -22, -22.7, 0.12, fx_Vortices
light.1 = 2, -22, 22.7, 0.12, fx_Vortices
light.2 = 4, 23.5, 0, 1.0, fx_vclight
light.3 = 3, -22.7, 0, 2.78, fx_navwhi
light.4 = 3, -9.0, -23.0, 0.23, fx_navred
light.5 = 3, -9.0, 23.0, 0.23, fx_navgre
light.6 = 3, -9.0, 23.0, 0.23, fx_strobe
light.7 = 3, -9.0, -23.0, 0.23, fx_strobe
light.8 = 9, -12,  -2.50,  0.65, fx_ALPHA_CF105_exh
light.9 = 9, -12,   2.60,  0.65, fx_ALPHA_CF105_exh
light.10 = 9, -12,  -2.50,  0.20, fx_Alpha_CF105_AB
light.11 = 9, -12,   2.60,  0.20, fx_Alpha_CF105_AB
light.12 = 7, -12,  -2.50,  0.65, fx_ALPHA_CF105_exh1
light.13 = 7, -12,   2.60,  0.65, fx_ALPHA_CF105_exh1


[GeneralEngineData]
engine_type= 1
fuel_flow_scalar= 1.400
engine.0 = -17.200, -1.600, 0.000
engine.1 = -17.200, 1.600, 0.000
min_throttle_limit=0.000000

[smokesystem]
smoke.0 = -12.00, -22.00, -2.50, fx_ALPHA_B1B_smoke
smoke.1 = -12.00, -22.00, 2.60, fx_ALPHA_B1B_smoke


[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
contrail = fx_contrail_l

[fuel]

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

fuel_type = 2
number_of_tank_selectors = 1

Center1 = 0, 0, 0, 4662, 3
electric_pump=0


[contact_points]
static_pitch = 1.6
static_cg_height = 7.66
max_number_of_points = 7

point.0 = 1, 14.8, 0, -8.3, 2000, 0, 1.1, 30, 0.11, 3, 0.8, 5, 5, 0, 260, 300
point.1 = 1, -1.2, -6.3, -8.1, 2500, 1, 2.2, 0, 0.5, 2.5, 0.85, 5, 5, 2, 260, 300
point.2 = 1, -1.2, 6.3, -8.1, 2500, 2, 2.2, 0, 0.5, 2.5, 0.85, 5, 5, 3, 260, 300
point.3 = 2.000, -12.128, -22.948, 0.082, 1500.000, 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, -12.128, 22.749, 0.198, 1500.000, 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, -20.5892, 0, -2.9939, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 42.7867, 0, -2.6306, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
gear_system_type=1


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


[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0,0,0,3.5813,0.7699,0.7699,0.6462,4.0485,1.5398,1.5398
//ACM_AREAW2// 1.2924,4.5156,2.3103,2.3103,1.9385,4.9828,3.0803,3.0803,2.5848,5.4499
//ACM_AREAW3// 3.8506,3.8506,3.2309,5.9169,4.6206,4.6206,3.8770,6.3842,5.3906,5.3906
//ACM_AREAW4// 4.5233,6.8512,6.1609,6.1609,5.1697,7.3185,6.9310,6.9310,5.8158,7.7856
//ACM_AREAH1// 0,0,0,2.8712,0.4785,0.4785,0.4620,3.1895,0.9570,0.9570
//ACM_AREAH2// 0.9240,3.5083,1.4356,1.4356,1.3861,3.8268,1.9141,1.9141,1.8480,4.1454
//ACM_AREAH3// 2.3926,2.3926,2.3104,4.4639,2.8712,2.8712,2.7727,4.7824,3.3496,3.3496
//ACM_AREAH4// 3.2348,5.1009,3.8282,3.8282,3.6967,5.4196,4.3067,4.3067,4.1588,5.7382
//ACM_AREAV1// 0,0,0,2.8573,0.3174,0.3174,0.4368,3.0657,0.6348,0.6348
//ACM_AREAV2// 0.8737,3.2741,0.9524,0.9524,1.3107,3.4825,1.2697,1.2697,1.7479,3.6909
//ACM_AREAV3// 1.5872,1.5872,2.1849,3.8993,1.9048,1.9048,2.6217,4.1076,2.2223,2.2223
//ACM_AREAV4// 3.0587,4.3161,2.5397,2.5397,3.4958,4.5244,2.8573,2.8573,3.9328,4.7329
//ACM_CAREAW1// 3.4655,3.4655,4.6985,5.4148,3.8506,3.8506,5.0215,5.7020,4.2357,4.2357
//ACM_CAREAW2// 5.3446,5.9895,4.6206,4.6206,5.6679,6.2768,5.0057,5.0057,5.9910,6.5640
//ACM_CAREAW3// 5.3906,5.3906,6.3140,6.8512,5.7758,5.7758,6.6373,7.1387,6.1609,6.1609
//ACM_CAREAW4// 6.9604,7.4257,6.5460,6.5460,7.2835,7.7132,6.9310,6.9310,7.6065,8.0003
//ACM_CAREAH1// 0,0,1.4356,2.8712,0.4785,0.4785,1.8976,3.2613,0.9570,0.9570
//ACM_CAREAH2// 2.3598,3.6517,1.4356,1.4356,2.8217,4.0422,1.9141,1.9141,3.2839,4.4324
//ACM_CAREAH3// 2.3926,2.3926,3.7460,4.8228,2.8712,2.8712,4.2083,5.2132,3.3496,3.3496
//ACM_CAREAH4// 4.6704,5.6034,3.8282,3.8282,5.1325,5.9938,4.3067,4.3067,5.5946,6.3842
//ACM_CAREAV1// 0,0,0.7142,2.1428,0.3174,0.3174,1.1512,2.4656,0.6348,0.6348
//ACM_CAREAV2// 1.5880,2.7883,0.9524,0.9524,2.0250,3.1110,1.2697,1.2697,2.4621,3.4337
//ACM_CAREAV3// 1.5872,1.5872,2.8991,3.7564,1.9048,1.9048,3.3361,4.0791,2.2223,2.2223
//ACM_CAREAV4// 3.7732,4.4018,2.5397,2.5397,4.2101,4.7245,2.8573,2.8573,4.6469,5.0472
wing_area = 660.930
wing_span = 46
wing_root_chord = 21.77
wing_dihedral = -4
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 0.883
wing_winglets_flag = 0
wing_sweep = 40
wing_pos_apex_lon = 11.89
wing_pos_apex_vert = 1.85
htail_area = 145.000
htail_span = 28.26
htail_pos_lon = -8.32
htail_pos_vert = 0
htail_incidence = -0.5
htail_sweep = 48
vtail_area = 112.000
vtail_span = 9.35
vtail_sweep = 54
vtail_pos_lon = -6.33
vtail_pos_vert = 2.16
elevator_area = 103.000
aileron_area = 26.000
rudder_area = 56.000
elevator_up_limit = 27.915
elevator_down_limit = 19.939
aileron_up_limit = 19.939
aileron_down_limit = 14.954
rudder_limit = 24.000
elevator_trim_limit = 18.000
spoiler_limit = 59.989
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 150
electric_always_available = 0

[direction_indicators]
direction_indicator.0=3,0 

[TurbineEngineData]
fuel_flow_gain= 0.003
inlet_area= 5.000 
rated_N2_rpm= 29920.000 
static_thrust= 19400.000 
afterburner_available= 1 
reverser_available= 0.000 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=2000.000000 
autothrottle_available= 1 
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
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

[jet_engine]
thrust_scalar=1.0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=0.505
yaw_stability=1.175
parasite_drag_scalar=1.000
induced_drag_scalar=1.002
elevator_effectiveness=0.709
aileron_effectiveness=1.002
rudder_effectiveness=0.500
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

 

[Reference Speeds]
flaps_up_stall_speed=179.000 
full_flaps_stall_speed=149.000 
cruise_speed=850.000 
max_indicated_speed=1200.000000
max_mach=2.820

[brakes]
toe_brakes_scale=0.7752
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0

[Views]
eyepoint=20.000000,0.000000,3.750000 

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 1
damaging-speed= 325.000
blowout-speed= 365.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.250, 0.000
flaps-position.2= 30.500, 0.000
flaps-position.3= 45.750, 0.000
flaps-position.4= 60.000, 0.000

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