[fltsim.0]
title=F4U-1D Corsair
sim=F4U1A_Corsair
model=
panel=
sound=
texture=
KB_checklists=f4u1a_corsair_check
[WEIGHT_AND_BALANCE]
empty_weight=8873 // (pounds)
reference_datum_position=0.00, 0.00, 0.00 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.00, 0.00, 0.00 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=170, -3.00, 0.00, 3.00 //Pilot - Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=11059.0
empty_weight_roll_MOI=7243.0
empty_weight_yaw_MOI=14484.0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[piston_engine]
power_scalar=1.0
[propeller]
thrust_scalar=1.0
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.12,0.11 ;Percent per second
[exits]
number_of_exits=1
exit_rate.0=0.4 ;Percent per second
[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position= -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.125 // 0.0 .. 1.0
extending-time=5 // seconds
flaps-position.0=0 // degrees, KIAS
flaps-position.1=16 // degrees, KIAS
flaps-position.2=32 // degrees, KIAS
flaps-position.3=48 // degrees, KIAS
flaps-position.4=64 // degrees, KIAS
flaps-position.5=80 // degrees, KIAS
damaging-speed=201 // KIAS
blowout-speed=305 // KIAS
[LSO]
LSOAdjustSpeed=1.2
[LIGHTS]
panel=0.00, 0.45, -2.00, fx_vclight
[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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//tail wheel
point.0= 1, -18.00, 0.00, -3.35, 3200.0, 0, 0.50,180.0, 0.25, 2.5, 0.90, 1.0, 4.00, 0, 0, 200
//left wheel
point.1= 1, 1.80, -5.93, -7.65, 2200.0, 1, 1.35, 0, 0.54, 2.5, 0.76, 5.5, 4.50, 2, 0, 200
//right wheel
point.2= 1, 1.80, 5.93, -7.65, 2200.0, 2, 1.35, 0, 0.54, 2.5, 0.76, 5.5, 4.50, 3, 0, 200
//left wing
point.3= 2, 0.00, -20.00, -1.25, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5
//Right wing
point.4= 2, 0.00, 20.00, -1.25, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6
//tail
point.5= 2, -20.25, 0.00, -1.66, 2400.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 9
//belly
point.6= 2, 5.41, 0.00, -3.50, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 4
//left gull
point.7= 2, 0.00, -5.43, -3.75, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5
//right gull
point.8= 2, 0.00, 5.43, -3.75, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6
static_pitch=11.90 //degrees (pitch when loaded on ground)
static_cg_height=6.60 //(feet) altitude of CG when at rest (altitude when loaded on ground)
[Views]
eyepoint=-6.20, 0.00, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum
