[fltsim.0]
title=Stealth FA-37 Talon
sim=FA-37
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
kb_notes=
atc_id=NAVY007
atc_airline=NAVY
atc_flight_number=007
ui_manufacturer=Stealth
ui_type=F/A-37 Talon
ui_variation=VFA 115
ui_typerole=Military Jet
ui_createdby=Bruce Fitzgerald
atc_heavy=0
visual_damage=1
atc_type=Stealth
atc_model=F/A-37
Description=

// ------------

[General]
atc_type=Stealth
atc_model=F/A-37
Performance=
Category=airplane

// --weight and balance

[Weight_And_Balance]
reference_datum_position= 0.00,0.0,0.0
empty_weight_CG_position=-2.19,0.0,0.0
CG_forward_limit=5.0
CG_aft_limit=   -5.0
empty_weight=12982.0
max_gross_weight=19000.0
max_number_of_stations=50
station_load.0=170.0,14.3,0.0,0.0
//Moments of Inertia
empty_weight_roll_MOI=25313.5
empty_weight_pitch_MOI=82291.3
empty_weight_yaw_MOI=81477.9
empty_weight_coupled_MOI=0.0

[Fuel]
LeftMain= -3.13,-8.4,0.0,150.0,0.0
RightMain=-3.13, 8.4,0.0,150.0,0.0
Center1=   0.00, 0.0,0.0,300.0,0.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=1


// --geometries

[contact_points]
//0  Class 0-none 1-wheel 2-scrape point 3-skid 4-float 5-water rudder
//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/Water Rudder Effectiveness (0=Undamped,1=Critically Damped)/1.0=normal
//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)
//========0====1====2=======3====4====5==6===7====8====9====10====11===12==13=14=15==
point.0 = 1, 19.5, 0.00,  -6.6, 8662, 0, 1, 60, 0.25, 0.3, 0.94, 3.5, 3.5,  0, 0, 0
point.1 = 1, -5.9,-5.10,  -6.8, 8662, 1, 1,  0, 0.75, 0.2, 0.58, 3.5, 3.5,  0, 0, 0
point.2 = 1, -5.9, 5.10,  -6.8, 8662, 2, 1,  0, 0.75, 0.2, 0.58, 3.5, 3.5,  0, 0, 0
//
static_pitch = 0.0
static_cg_height = 6.7
max_number_of_points = 7
gear_system_type=0

[airplane_geometry]
wing_area               = 400.0                 //Square feet
wing_span               = 37.4                  //Feet
wing_root_chord         = 13.3                  //Feet
wing_dihedral           = 2.5                   //Degrees
wing_incidence          = -3.0                  //Degrees
wing_twist              = -1.5                  //Degrees
oswald_efficiency_factor= 0.85                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 20.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = -27.7                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 88.26                 //Square feet
htail_span              = 21.6                  //Feet
htail_pos_lon           = -47.6                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 42.8                  //Degrees, horizontal tail leading edge
vtail_area              = 1050                  //Square feet
vtail_span              = 7.8                   //Feet, tip to body
vtail_sweep             = 45.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -42.3                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 4.5                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 27.0                  //Square feet
aileron_area            = 13.5                  //Square feet
rudder_area             = 27.3                  //Square feet
elevator_up_limit       = 19.0                  //Degrees
elevator_down_limit     = 19.5                  //Degrees
aileron_up_limit        = 19.0                  //Degrees
aileron_down_limit      = 18.0                  //Degrees
rudder_limit            = 45.0  // used for nosewheel animation                //Degrees
elevator_trim_limit     = 15.0                  //Degrees
spoiler_limit           = 80.0                  //Degrees
spoiler_extension_time  = 0.4                   //Seconds
spoilerons_available    = 1                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons= 0.0                   //Minimum flap handle position when spoilerons activate
auto_spoiler_available   = 0
positive_g_limit_flaps_up  =  37.5               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=  37.5               //Design G load tolerance (positive, flaps down) 
negative_g_limit_flaps_up  = -35.0               //Design G load tolerance (negative, flaps up) 
negative_g_limit_flaps_down= -35.0               //Design G load tolerance (negative, flaps down) 


// --visuals

[CameraDefinition.0]
Title = "Tail"
Guid = {5D23AC3D-6949-4dae-8FB7-E913545D1641}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .90
ShowWeather = Yes
InitialXyz = 0, 5.3, -34.0
InitialPbh = 3, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[Views]
eyepoint=0,0,0  // VC origin datum
zoom=1.0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=4,   0.0,    0.0,   0.0,  fx_litewash // cockpit lighting interior view
light.1=4,  28.5,    2.0,   4.0,  fx_litewash // cockpit lighting exterior view
// bcn,nav,strobe are imbedded in model

[SMOKESYSTEM]
smoke.0=-22.50,  2.0, -0.7, fx_F16burner // FSX only - gauge controlled - autosmoke
smoke.1=-22.50, -2.0, -0.7, fx_F16burner // FSX only - gauge controlled - autosmoke

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

// --dynamic vars

[flight_tuning]
cruise_lift_scalar     = 0.8
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 1.0
rudder_effectiveness   = 0.5
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.3
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

// --airframe

[brakes]
toe_brakes_scale=8.000061
parking_brake=1

[Flaps.0]
// wings
type=1
span-outboard=0.45
extending-time=3.0
system_type=1
damaging-speed=0.0
blowout-speed=0.0
lift_scalar=0.1
drag_scalar=0.4
pitch_scalar=0.0
flaps-position.0= 0.0,0.0
flaps-position.1= 82.0,0.0
flaps-position.2= 82.0,0.0
flaps-position.3= 82.0,0.0

[Flaps.1]
// dunno, but needs to be here
type=2
span-outboard=0.45
extending-time=3.0
system_type=1
damaging-speed=980.0
blowout-speed=990.0
lift_scalar=0.1
drag_scalar=0.1
pitch_scalar=0.0
flaps-position.0= 0.0,0.0
flaps-position.1= 0.0,0.0
flaps-position.2= 0.0,0.0
flaps-position.3= 0.0,0.0

[Flaps.2]
// flappy flaps
type=1
span-outboard=0.45
extending-time=5.0
system_type=1
damaging-speed980.0
blowout-speed=990.0
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=0.0
flaps-position.0= 0.0,0.0
flaps-position.1= 0.0,0.0
flaps-position.2= 12.0,0.0
flaps-position.3= 25.0,0.0

[Flaps.3]
// stabs
type=2
span-outboard=0.45
extending-time=5.0
system_type=1
damaging-speed=0.0
blowout-speed=0.0
lift_scalar=0.1
drag_scalar=0.1
pitch_scalar=0.0
flaps-position.0= 0.0,0.0
flaps-position.1= 25.0,0.0
flaps-position.2= 30.0,0.0
flaps-position.3= 35.0,0.0
[Reference Speeds]

flaps_up_stall_speed=135.000
full_flaps_stall_speed=76.0
cruise_speed=660.0
max_indicated_speed=2800.000000
max_mach=4.300000

[Folding_wings]
wing_fold_system_type=4
fold_rates=0.12,0.13

[TailHook]
tailhook_length=5.83
tailhook_position=-14.6, 0.0,-0.8
cable_force_adjust=1.0

[launch_assistance]
launch_bar_pivot = 19.5, 0.00,  -5.0
launch_bar_lug =   20.5, 0.00,  -6.6

[Exits]
number_of_exits=2
exit_rate.0=0.8

// --powerplant

[GeneralEngineData]
engine_type = 1
Engine.0 = -15.8, -2.5, -0.1
Engine.1 = -15.8,  2.5, -0.1
fuel_flow_scalar        = 0.01
min_throttle_limit = 0

[TurbineEngineData]
fuel_flow_gain          = 0.006
inlet_area              = 3.2895
rated_N2_rpm            = 21728
static_thrust           = 15000
afterburner_available   = 6  
afterburner_throttle_threshold = 0.90 
reverser_available      = 0 
ThrustSpecificFuelConsumption = 0.71
AfterBurnThrustSpecificFuelConsumption = 1.44    

[jet_engine]
thrust_scalar = 1.0

// --instrumentation

[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=1,0,1
Adf.1=1
Transponder.1=1
Marker.1=1
                      
[Autopilot]
autopilot_available=1
use_no_default_pitch=1
use_no_default_bank=1
flight_director_available=1
default_vertical_speed=500.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.0
pitch_takeoff_ga=8.0
default_pitch_mode=0
default_bank_mode=0
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

[Direction_indicators]
direction_indicator.0=3,0

[turn_indicators]
turn_indicator.0=1,0

[attitude_indicators]
attitude_indicator.0=1

[stall_warning]
type=1
stick_shaker=1

[GPWS] 
max_warning_height = 0 
sink_rate_fpm = -5000 
excessive_sink_rate_fpm = -30000 
climbout_sink_rate_fpm = -100 
flap_and_gear_sink_rate_fpm= -10000

// --systems

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=4500.000000

[Electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=150.0
electric_always_available = 1

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

[pitot_static]
pitot_heat=1.000000

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[deice_system]
structural_deice_type=0

// --peripherals

[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=8900                ; 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

[Keyboard_response]
elevator=250.0, 500.0
aileron= 250.0, 500.0
rudder=  250.0, 500.0