[fltsim.0] title=F4U-1C 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