////////////////////////////////////////////
     //                                        //
     //          Dassault Mirage IV P          //
     //              pour FS 2004              //
     //           par Roland Laborie           //
     //                                        //
     //            Dynamique de vol            //
     //        de Jean-Pierre Bourgeois        //
     //                                        //
     //           version bg17 mod 05          //
     //             08/02/2008                 //
     //                                        //
     //                                        //
     ////////////////////////////////////////////
//
// 08/08/2007  Remis les effets, fumйes et feux originaux de Rollus
// 12/08/2007  Version bg02 + carburant dйfinitif
// 14/08/2007  Section Autopilot rectifiйe
// 15/08/2007  Fichier air -bg-04
// 20/08/2007  Fichier air -bg-05 
// 21/08/2007  Fichier air -bg-06
// 23/08/2007  Modifs en section autopilot (autothrottle)
// 23/08/2007  Fuel pump = 2 (1 par moteur) et PA (navigation)
// 26/08/2007  Fichier air -bg-07, modif eyepoint
// 27/08/2007  engine_generator_map = 1,1 au lieu de 1,0
// 31/08/2007  engine_map = 1,1,0,0  dans l'hydraulique
// 02/10/2007  adaptation mdl du 01/10
// 02/10/2007  modif param points contact
// 02/10/2007  modif feux de position
// 03/10/2007  rajout repli des ailes pour parachute
// 06/10/2007  modif feux de position
// 09/10/2007  mofifs P oil et Hydr, fichier air -10
// 10/10/2007  modifs AF, modifs mineurs fichier air -11
// 11/10/2007  ajust. param. trains atterr.
// 12/10/2007  modif effets de flammes des rйacteurs
// 19/10/2007  rajoutй max_contrail_temperature 
// 20/10/2007  adaptй freinage parachute (reverses)
// 16/12/2007  instruments - mise а jour (Jean Pierre Langer)
// 21/12/2007  Fichier air -bg-15 (+JATO) (Jean Pierre Bourgeois)
// 21/12/2007  MDL (modиle exterieur) - (aircraft.cfg :eye-point) 2 livrйes (ALU-blanc) (Laborie Roland)
// 20/01/2008  Finalisation fichier air.... enfin j'espиre !
// 09/02/2008  Ajustement distance franchissable



[fltsim.0]
title=Dassault Mirage IV P 
sim=MirageIV-bg19
model=
panel=     //ori
sound=
texture=
kb_checklists=MP4_check
ui_manufacturer=Dassault
ui_type=Mirage IV P
ui_variation=Gascogne 
description=FRENCH AIR FORCE \Gascogne panel ori
atc_id=F-GYBZ
atc_type=DASSAULT
atc_model=MIR4
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0


[fltsim.1]
title=Dassault Mirage IV P2
sim=MirageIV-bg19
model=
panel=
sound=
texture=AX
kb_checklists=MP4_check
ui_manufacturer=Dassault
ui_type=Mirage IV P
ui_variation=AX-Bretagne
description=FRENCH AIR FORCE \Bretagne
atc_id=F-GYBZ
atc_type=DASSAULT
atc_model=MIR4
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0




[fltsim.2]
title=Dassault Mirage IV P3 
sim=MirageIV-bg19
model=
panel=
sound=
texture=UN
kb_checklists=MP4_check
ui_manufacturer=Dassault
ui_type=Mirage IV P 
ui_variation=UN
description=FRENCH AIR FORCE \United Nations
atc_id=F-GYBZ
atc_type=DASSAULT
atc_model=MIR4
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0


[fltsim.3]
title=Dassault Mirage IV P4 
sim=MirageIV-bg19
model=
panel=
sound=
texture=celebration
kb_checklists=MP4_check
ui_manufacturer=Dassault
ui_type=Mirage IV P 
ui_variation=celebration
description=FRENCH AIR FORCE \celebration
atc_id=F-GYBZ
atc_type=DASSAULT
atc_model=MIR4
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0


[fltsim.4]
title=Dassault Mirage IV P5 
sim=MirageIV-bg19
model=
panel=
sound=
texture=Alu
kb_checklists=MP4_check
ui_manufacturer=Dassault
ui_type=Mirage IV P 
ui_variation=Alu
description=FRENCH AIR FORCE \Alu
atc_id=F-GYBZ
atc_type=DASSAULT
atc_model=MIR4
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0


[fltsim.5]
title=Dassault Mirage IV P6 
sim=MirageIV-bg19
model=
panel=
sound=
texture=Blanc
kb_checklists=MP4_check
ui_manufacturer=Dassault
ui_type=Mirage IV P 
ui_variation=Blanc
description=FRENCH AIR FORCE \blanc
atc_id=F-GYBZ
atc_type=DASSAULT
atc_model=MIR4
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[fltsim.6]
title=Dassault Mirage IV P7 
sim=MirageIV-bg19J
model=JATO
panel=
sound=
texture=Alu
kb_checklists=MP4_check
ui_manufacturer=Dassault
ui_type=Mirage IV P 
ui_variation=Alu-JATO
description=FRENCH AIR FORCE \Alu
atc_id=F-GYBZ
atc_type=DASSAULT
atc_model=MIR4
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[General]
editable=0 
performance="Vitesse de croisiиre\t\nMach 2,3        1317 noeuds      2371 km/h\n\nMotorisation\t\     29540 livres de poussйe\n\nAutonomie maximale\t\n7 200 nm          8287 mi \t4 074 km\n\nPlafond pratique\t\n65 616 pieds           20 000 m\nLongueur\t\n76,5 pieds\t               23,32 m\n\nEnvergure\t\n38,84 pieds\t              11,84 m\n\nHauteur\t\n17,78 pieds\t              5,42 m\n\nNombre de places\t\1 pilote 1 navigateur 
CARACTЙRISTIQUES  M IVp
Dimensions Longueur .................................23.32 m
Envergure ................................11.84 m
Hauteur ....................................  5.42 m
Masse а vide йquipй ..............14.50  t
Masse max. au dйcollage.........33 t 
Motorisation Deux turborйacteurs SNECMA ATAR 9K13 avec postcombustion qui dйlivrent chacun :
                                            - 4.820 kg а sec
                                            - 6.700 kg avec PC
Carburant TRO
12 fusйes JATO de 420 kg de poussйe chacune apportent une poussйe totale supplйmentaire de 5.040 kg  
Performances Vitesse .........................................mach 2.2
Plafond opйrationnel .................20.000 m
Rayon d'action .............................4.000 km 
Йquipements Radar DOPPLER
Centrale gyroscopique
Pilote automatique
Systиme de ravitaillement en vol
Contre-mesures йlectroniques
Deux siиges йjectables Martin-Baker BM4 
;-----------------------------------------------------------------------

[weight_and_balance]

// ACM V2.5
max_gross_weight = 73799
empty_weight = 32500
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -2, 0, 2
empty_weight_pitch_MOI = 475000
empty_weight_roll_MOI = 265000
empty_weight_yaw_MOI = 485000
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 1

station_load.0 = 4410, -2, 0, 2


[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, -17.35, -18.65,  1.05, fx_navred
light.1  = 3, -17.35,  18.65,  1.05, fx_navgre
light.2  = 3, -28.80,   0.40, 11.75, fx_navwhi
light.3  = 3, -28.80,  -0.40, 11.75, fx_navwhi
light.4  = 2, -17.35, -18.65,  1.25, fx_strobe
light.5  = 2, -17.35,  18.65,  1.25, fx_strobe
light.6  = 2,  10.00,   0.00,  5.10, fx_strobe
light.7  = 4,  25.31,   0.00,  1.69, fx_vclight
// Left reactor
light.8  = 9, -26.78,  -2.00,  2.50, fx_mirage_BURN_ONE
light.9  = 9, -27.00,  -2.00,  2.50, fx_mirage_BURN_TWO
light.10 = 9, -31.70,  -2.00,  2.50, fx_mirage_GLITTER
light.11 = 8, -33.63,  -2.00,  2.50, fx_mirage_TORCH_FLAM
// Right reactor
light.12 = 7, -26.78,   2.00,  2.50, fx_mirage_BURN_ONE
light.13 = 7, -27.00,   2.00,  2.50, fx_mirage_BURN_TWO
light.14 = 7, -31.70,   2.00,  2.50, fx_mirage_GLITTER
light.15 = 6, -33.63,   2.00,  2.50, fx_mirage_TORCH_FLAM

[GeneralEngineData]

engine_type = 1                          //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
fuel_flow_scalar = 1.05    //1.28     //2.2                   //Scalar for fuel flow efficiency
min_throttle_limit = -0.40               //Minimum percent throttle.  Generally negative for turbine reverser
engine.0 = -18, -1.5, 2,                 //(feet) longitudinal, lateral, vertical distance from reference datum
engine.1 = -18,  1.5, 2,                 //(feet) longitudinal, lateral, vertical distance from reference datum
max_contrail_temperature = -30           //Temperature (deg C) below which contrails may appear

[smokesystem]
//smoke.0 = 0.0, -17.0,  0.0,  fx_smoke_RFN
smoke.1 = -30, -40.21, 2.38, fx_contrail_s.fx
smoke.2 = -30, -40.21, -2.59, fx_contrail_s.fx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1

[fuel]

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

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = -2, -1.2, 2, 791, 0
LeftAux = -2, -5, 2, 508, 0
LeftTip = -2, 0, 2, 488, 0
RightMain = -2, 1.2, 2, 791, 0
RightAux = -2, 5, 2, 508, 0
RightTip = -2, 0, 2, 488, 0
External1 = -2, -7, 2, 688, 0
External2 = -2, 7, 2, 688, 0


[contact_points]
static_pitch =  4.2
static_cg_height = 5.0     //5.5
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7

point.0 = 1, 19, 0, -6.5, 1574, 0, 0.68287, 30, 0.30573, 1, 0.781503, 5, 5, 0, 0, 0
point.1 = 1, -7.6, -8, -5.05, 1574, 1, 0.68287, 0, 0.405771, 1, 0.781504, 5, 5, 2, 0, 0
point.2 = 1, -7.6, 8, -5.05, 1574, 2, 0.68287, 0, 0.405771, 1, 0.781504, 5, 5, 3, 0, 0
point.3 = 2, -18.4859, -19.3633, 1.3996, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -18.5897, 19.5697, 1.3729, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -29.5079, -0.2117, 2.245, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 44.308, 0, -1.5798, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
//ACM_AREAW1// 0,0,0,4.1655,0.6491,0.6491,0,3.9572,1.2982,1.2982
//ACM_AREAW2// 0,3.7490,1.9471,1.9471,0,3.5406,2.5964,2.5964,0,3.3324
//ACM_AREAW3// 3.2455,3.2455,0,3.1242,3.8945,3.8945,0,2.9158,4.5437,4.5437
//ACM_AREAW4// 0,2.7076,5.1928,5.1928,0,2.4993,5.8420,5.8420,0,2.2908
//ACM_AREAH1// 0,0,0,1.6933,0.2822,0.2822,0,1.6086,0.5644,0.5644
//ACM_AREAH2// 0,1.5240,0.8464,0.8464,0,1.4392,1.1288,1.1288,0,1.3545
//ACM_AREAH3// 1.4111,1.4111,0,1.2697,1.6933,1.6933,0,1.1849,1.9752,1.9752
//ACM_AREAH4// 0,1.1006,2.2576,2.2576,0,1.0160,2.5399,2.5399,0,0.9312
//ACM_AREAV1// 0,0,0,3.1082,0.3452,0.3452,0,2.8596,0.6905,0.6905
//ACM_AREAV2// 0,2.6110,1.0361,1.0361,0,2.3622,1.3811,1.3811,0,2.1136
//ACM_AREAV3// 1.7266,1.7266,0,1.8650,2.0722,2.0722,0,1.6160,2.4175,2.4175
//ACM_AREAV4// 0,1.3674,2.7629,2.7629,0,1.1188,3.1082,3.1082,0,0.8701
//ACM_CAREAW1// 2.9210,2.9210,2.0827,2.9158,3.2455,3.2455,2.0827,2.8742,3.5701,3.5701
//ACM_CAREAW2// 2.0827,2.8326,3.8945,3.8945,2.0827,2.7908,4.2192,4.2192,2.0827,2.7492
//ACM_CAREAW3// 4.5437,4.5437,2.0827,2.7076,4.8681,4.8681,2.0827,2.6658,5.1928,5.1928
//ACM_CAREAW4// 2.0827,2.6243,5.5173,5.5173,2.0827,2.5826,5.8420,5.8420,2.0827,2.5408
//ACM_CAREAH1// 0,0,0.8464,1.6933,0.2822,0.2822,0.8464,1.6510,0.5644,0.5644
//ACM_CAREAH2// 0.8464,1.6086,0.8464,0.8464,0.8464,1.5663,1.1288,1.1288,0.8464,1.5240
//ACM_CAREAH3// 1.4111,1.4111,0.8464,1.4816,1.6933,1.6933,0.8464,1.4392,1.9752,1.9752
//ACM_CAREAH4// 0.8464,1.3969,2.2576,2.2576,0.8464,1.3545,2.5399,2.5399,0.8464,1.3121
//ACM_CAREAV1// 0,0,0.7770,2.3310,0.3452,0.3452,0.7770,2.2067,0.6905,0.6905
//ACM_CAREAV2// 0.7770,2.0826,1.0361,1.0361,0.7770,1.9579,1.3811,1.3811,0.7770,1.8336
//ACM_CAREAV3// 1.7266,1.7266,0.7770,1.7094,2.0722,2.0722,0.7770,1.5851,2.4175,2.4175
//ACM_CAREAV4// 0.7770,1.4608,2.7629,2.7629,0.7770,1.3365,3.1082,3.1082,0.7770,1.2122
wing_area = 840.000000
wing_span = 38.33
wing_root_chord = 37.61
wing_dihedral = 0
wing_incidence = -0.494385
wing_twist = -0.999756
oswald_efficiency_factor = 0.38
wing_winglets_flag = 0
wing_sweep = 60
wing_pos_apex_lon = 14.82
wing_pos_apex_vert = 1.33
htail_area = 80.000000
htail_span = 16.62
htail_pos_lon = -22.68
htail_pos_vert = 0.80
htail_incidence = 0.000000
htail_sweep = 0
vtail_area = 80.000000
vtail_span = 9.75
vtail_sweep = 60
vtail_pos_lon = -11.14
vtail_pos_vert = 5.23
elevator_area = 20.000000
aileron_area = 21.000000
rudder_area = 20.400000
elevator_up_limit = 20
elevator_down_limit = 20
aileron_up_limit = 20
aileron_down_limit = 20
rudder_limit = 23.491270
elevator_trim_limit = 20.000
spoiler_limit = 60
aileron_to_spoileron_gain = 0.000000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons = 0.000000
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
fuel_transfer_pump = 0, 10, 17

[flight_tuning]
cruise_lift_scalar=1.000 
parasite_drag_scalar=1.000 
induced_drag_scalar=1.000 
elevator_effectiveness=1.000 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
pitch_stability=1.000 
roll_stability=1.000 
yaw_stability=1.000 
elevator_trim_effectiveness=1.000 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 
;-----------------------------------------------------------------------

[gear_warning_system]
gear_warning_available = 0    //Normal
pct_throttle_limit =   0.1     //Percent throttle that activates warning
flap_limit_idle    =  60.0     //Flap angle that activates warning at idle
flap_limit_power   =  60.0     //Flap angle that activates warning at above idle

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2,3,4

[Views]
//eyepoint=25.0, 0, 3.8
eyepoint=25.0, 0 , 3.9
;-----------------------------------------------------------------------

[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 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[jet_engine]
thrust_scalar=1.0 
;-----------------------------------------------------------------------

[TurbineEngineData]
fuel_flow_gain=0.02 
inlet_area=3.50            //12.000
rated_N2_rpm=8400.000 
static_thrust=11060   //   poussйe sec 15810  PC  ratio 1.43
afterburner_available=1 
reverser_available=1 
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear
;-----------------------------------------------------------------------

[Reference Speeds]
flaps_up_stall_speed=140.000 
full_flaps_stall_speed=140.000 
cruise_speed=500.000 
max_mach=2.2
max_indicated_speed= 650.000
;-----------------------------------------------------------------------

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_pitch_mode=0  
max_pitch=20.0                     // The maximum pitch angle in degrees that the autopilot will command either up or down.
max_pitch_acceleration=5.0         // Max angular pitch acceleration (°/s^2) that the autopilot will command up or down.  
max_pitch_velocity_lo_alt=3.0      // Max angular pitch velocity (°/s) autopilot will command when at low altitude (<20000)
max_pitch_velocity_hi_alt=1.5      // Max angular pitch velocity (°/s) autopilot will command when at high altitude (>28000)
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
default_vertical_speed=1000        // Default vertical speed (ft/s) autopilot will command when selecting a large altitude change.  
default_bank_mode =0  
max_bank=30.0                      // The maximum bank angle in degrees that the autopilot will command either left or right.  
max_bank_acceleration=6.0          // Max angular bank acceleration (°/s^2) that the autopilot will command left or right.  
max_bank_velocity=12.00            // The maximum angular bank velocity (°/s) which the autopilot will command left or right.
yaw_damper_gain = 4.0              // The proportional gain on the yaw damper’s yaw rate error.  
autothrottle_available=1           // 0 = no autothrottle
autothrottle_arming_required=0     //
autothrottle_max_rpm =100 //99.8         // Sets the maximum engine speed, in percent, that the autothrottle will attempt to maintain.
autothrottle_takeoff_ga= 0         // Setting this flag to 1 enables takeoff / go-around operations with the autothrottle.
pitch_takeoff_ga=15                //
max_throttle_rate=0.25             // Sets the maxi rate at which the autothrottle will move the throttle position.
                                   // Here, the maximum rate is set to 25% of the total throttle range per second
nav_proportional_control=24.00     // Proportional controller constant in lateral navigation modes.
nav_integrator_control=0.20        // Integral controller constant in lateral navigation modes.
nav_derivative_control=0.50        // Derivative controller constant in lateral navigation modes.
nav_integrator_boundary=6.00       // Max signal error, in degrees in which the integrator function is active. 
                                   // Here, integrator is active when error is between -5/+5° from centerline of navigation signal
nav_derivative_boundary=2.00       // Max signal error, in degrees in which the derivative function is active. 0 = no active
gs_proportional_control=25.0       // Proportional controller constant in glideslope mode.
gs_integrator_control=0.53         // Integral controller constant in glideslope mode. (=0.53 on B737-400)
gs_derivative_control=0.00         // Derivative controller constant in glideslope mode.
gs_integrator_boundary=0.70        // Max signal error (°) in which the glideslope integrator function is active. Here +-0.7°
gs_derivative_boundary=0.00        // Max signal error, in degrees in which the derivative function is active. 0 = no active

//default_pitch_mode=0
//default_bank_mode=0
//use_no_default_bank=1
//use_no_default_pitch=1
;-----------------------------------------------------------------------

[stall_warning]
type=1
stick_shaker=1
[exits]
number_of_exits = 2
exit_rate.0 = 0.2       
exit_rate.1=0.4
;-----------------------------------------------------------------------

[Flaps.0]
type= 1
span-outboard= 1
extending-time= 0.1
system_type= 0
damaging-speed= 2000
blowout-speed= 2000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0
flaps-position.1= 50
;-----------------------------------------------------------------------

[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
;-----------------------------------------------------------------------
[brakes]
parking_brake=1        //Parking brake available
toe_brakes_scale=0.8  //Brake scalar
auto_brakes=4
hydraulic_system_scalar=1  //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure
;-----------------------------------------------------------------------
[folding_wings]
wing_fold_system_type=4                      ;0=None
fold_rates= 0.8, 0.8                         ;Percent per second
;-----------------------------------------------------------------------

[TailHook]
tailhook_length=6.47
tailhook_position=-9.65, 0.00, -2.13
cable_force_adjust=1.0