[fltsim.0]
title=P47
sim=P47
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Republic
ui_type=P47
ui_variation=Blue camouflage
description=Vast numbers of p47D's strafed and bombed throughout the european and pacific theaters until the end of world war two. Republic's output of D models (12,602) is the largest total of one subtype of any fighter in history, total production of the "jug" amounting to 15,660. After World War II this aircraft was popularwith many air forces untill well into the 1950's
atc_heavy=0
atc_id=N96759
atc_airline=
atc_flight_number=
[General]
editable=0
atc_type=
atc_model=
performance=Max speed\n417 mph 671 km\/h @ 19,900 ft\n\nEngine\nPratt & Whitney R-2800-21 Double Wasp 18-cyl. two row radial air-cooled, 2,000 hp\n\nMax Weight\n12,700 lb 6,350 kg\n\nCeiling\n36,900 ft 11,247 m\n\nInitial climb rate\n2,800 ft\/min 881 m\/min\n\nRange\n1,596 mi 2,568 km\n2,215 mi 3,565 km with drop tanks
[forcefeedback]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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
[WEIGHT_AND_BALANCE]
empty_weight = 8873 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -3.0, 0.0, 3.0 //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
empty_weight_coupled_MOI= 0.0
max_gross_weight= 12259.000
[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
cylinder_displacement=155.560000
compression_ratio=6.700000
number_of_cylinders=18
max_rated_rpm=2700.000000
max_rated_hp=2000.000000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=52.999999
min_design_mp=1.000000
critical_altitude=21500.000000
emergency_boost_type=1
emergency_boost_mp_offset=10.000000
emergency_boost_gain_offset=0.660000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
[propeller]
thrust_scalar = 1.0
propeller_type=0
propeller_diameter=13.330000
propeller_blades=3
propeller_moi=62.170000
beta_max=65.000000
beta_min=13.000000
min_gov_rpm=1800.000000
prop_tc=0.010000
gear_reduction_ratio=2.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[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
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=900.0
autothrottle_available=0
pitch_takeoff_ga=8.0
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=0, 0
Nav.1=1, 0, 0
Nav.2=0, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=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
[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)
point.0= 1, -18.00, 0.00, -3.70, 3200.0, 0, 0.50,180.0, 0.25, 2.5, 0.90, 1.0, 4.00, 0, 0, 200 //tail wheel
point.1= 1, 1.80, -5.93, -8.50, 2200.0, 1, 1.35, 0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 2, 0, 200 //left wheel
point.2= 1, 1.80, 5.93, -8.50, 2200.0, 2, 1.35, 0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 3, 0, 200 //right wheel
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 //left 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 //Right wing
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 //tail
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 //belly
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 //left 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 //right gull
static_cg_height = 7.00 //(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch = 13.9 //degrees (pitch when loaded on ground)
[Views]
eyepoint= -6.2, 0.00, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum
[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]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -0.3, -20.4, -0.7, fx_navred ,
light.1=3, -0.3, 20.6, -0.7, fx_navgre ,
light.2=3, -22.3, -0.01, 7.4, fx_navwhi ,
light.3=2, -0.3, -20.4, -0.7, fx_strobe ,
light.6=2, -0.3, 20.6, -0.7, fx_strobe ,
light.7=2, -22.3, -0.01, 7.4, fx_strobe ,
panel=0.00, 0.45, -2.00, fx_vclight
[fuel]
Center1=-1.940000,0.000000,-0.500000,187.000000,0.000000
Center2=-1.940000,0.000000,-0.500000,50.000000,0.000000
LeftMain=-0.970000,-12.250000,-1.610000,62.000000,0.000000
RightMain=-0.970000,12.250000,-1.610000,62.000000,0.000000
External1=1.940000,0.000000,-3.870000,175.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
[airplane_geometry]
wing_area=314.000000
wing_span=41.000000
wing_root_chord=7.833333
wing_dihedral=13.595581
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.699202
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=24.000000
htail_span=11.000000
htail_pos_lon=-18.833333
htail_pos_vert=0.000000
htail_incidence=-0.999756
htail_sweep=0.000000
vtail_area=15.000000
vtail_span=4.415880
vtail_sweep=0.000000
vtail_pos_lon=-18.833333
vtail_pos_vert=0.583333
elevator_area=13.000000
aileron_area=20.400000
rudder_area=13.060000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=21.497376
aileron_down_limit=20.345731
rudder_limit=28.997394
elevator_trim_limit=19.996227
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[GeneralEngineData]
engine_type=0
Engine.0=7.000000,0.000000,0.000000
fuel_flow_scalar=1.000000
[Reference Speeds]
flaps_up_stall_speed=65.000000
full_flaps_stall_speed=52.000000
cruise_speed=288.724811
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
[direction_indicators]
direction_indicator.0=1,0
