[fltsim.0] title=F6F-3 Hellcat sim=F6F3_Hellcat model= panel= sound= texture= KB_checklists=f6f3_hellcat_check ui_manufacturer = Grumman ui_type = F6F-3 Hellcat ui_variation=U.S. Navy description=Simple, rugged, and deadly, yet easy to fly, the Hellcat was another product of the so-called Grumman Iron Works. It was a larger, heavier, faster, and more powerful refinement of Grumman's F4F Wildcat, and the first American fighter to exceed the performance of the Mitsubishi Zero. Its immense 18-cylinder, 2,000 horsepower radial engine gave it the power to dictate the terms of engagement. Its speed, maneuverability, high-altitude capability, and typical Grumman toughness made it a winner against all comers. [WEIGHT_AND_BALANCE] empty_weight = 9042 // (pounds) reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.0, 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 = 11442.32 //slug-ft^2 empty_weight_roll_MOI = 8056.44 //slug-ft^2 empty_weight_yaw_MOI = 15600.73 //slug-ft^2 empty_weight_coupled_MOI=0.00 max_gross_weight=13818.00 [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=155.5500 compression_ratio=6.700 number_of_cylinders=18 max_rated_rpm=2700.00 max_rated_hp=2000.00 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.03500 turbocharged=1 max_design_mp=54.00 min_design_mp=1.00 critical_altitude=23000.00 emergency_boost_type=1 emergency_boost_mp_offset=5.00 emergency_boost_gain_offset=0.400 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.20 idle_rpm_mechanical_efficiency_scalar=1.00 max_rpm_friction_scalar=1.00 idle_rpm_friction_scalar=0.800 [propeller] thrust_scalar = 1.0 propeller_type=0 propeller_diameter=13.0800 propeller_blades=3 propeller_moi=58.800 beta_max=65.00 beta_min=13.00 min_gov_rpm=1800.00 prop_tc=0.0100 gear_reduction_ratio=2.00 fixed_pitch_beta=0.00 low_speed_theory_limit=80.00 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.00 beta_feather=0.00 power_absorbed_cf=0.00 defeathering_accumulators_available=0 prop_reverse_available=0.00 minimum_on_ground_beta=0.00 minimum_reverse_beta=0.00 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.13 ;Percent per second [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [TailHook] tailhook_length=4 ;(feet) tailhook_position = -23.6, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1.0 [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [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, -19.00, 0.00, -3.98, 3200, 0, 0.40,180.0, 0.30, 2.5, 0.70, 1.0, 6.0, 0, 0, 235 point.1=1, 2.25, -5.60, -8.15, 2200, 1, 1.30, 0.0, 0.80, 2.5, 0.68, 5.0, 7.5, 2, 0, 235 point.2=1, 2.25, 5.60, -8.15, 2200, 2, 1.30, 0.0, 0.80, 2.5, 0.68, 5.0, 7.5, 3, 0, 235 point.3=2, 0.00,-20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4=2, 0.00, 20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5=2, -19.00, 0.00, -1.66, 2400, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6=2, 2.41, 0.00, -2.08, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_cg_height = 6.87 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch = 10.31 //degrees (pitch when loaded on ground) gear_system_type=1 [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=191 // KIAS blowout-speed=290 // KIAS [Views] eyepoint=-3.1,0.050000,5.71 [LSO] LSOAdjustSpeed=1.05 [LIGHTS] panel=0.00, 0.75, -0.80, fx_vclight light.0=3, 0.0, -22.40, 0.80, fx_navred light.1=3, 0.0, 22.40, 0.80, fx_navgre light.2=3, -23.7, 0.00,-1.00, fx_navwhi [General] performance=Weight: 9,042\/11,381 lbs\nEngine: Pratt & Whitney R-2800-10\nDouble Wasp 18-cyl. radial air-\ncooled, 2,000 hp\nMax speed: 376 mph @ 17,300 ft\nCeiling: 38,400 ft\nInitial climb rate: 3,500 ft\/min\nRange: 1,090 miles or\nwith drop tanks, 1,590 miles\n [fuel] Center1= -3.900, 0.00, -1.600, 75.00, 0.00 LeftMain= -0.350,-1.20, -1.200, 87.50, 0.00 RightMain=-0.350, 1.200, -1.200, 87.50, 0.00 External1= 2.300, 0.000, -4.400,150.00, 0.00 fuel_type=1 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=334.00 wing_span=43.00 wing_root_chord=10.10 wing_dihedral=10.398560 wing_incidence=0.999756 wing_twist=0.00 oswald_efficiency_factor=0.699251 wing_winglets_flag=0 wing_sweep=10.00 wing_pos_apex_lon=3.30 wing_pos_apex_vert=-1.00 htail_area=24.00 htail_span=18.20 htail_pos_lon=-17.60 htail_pos_vert=0.70 htail_incidence=-0.999756 htail_sweep=15.00 vtail_area=15.00 vtail_span=4.30 vtail_sweep=0.00 vtail_pos_lon=-17.80 vtail_pos_vert=2.10 elevator_area=13.00 aileron_area=20.400 rudder_area=13.0600 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=0.00 spoilerons_available=0 aileron_to_spoileron_gain=0.00 min_ailerons_for_spoilerons=0.00 min_flaps_for_spoilerons=0.00 [brakes] toe_brakes_scale=0.48420 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.00 flap_limit_power=0.00 flap_limit_idle=0.00 [GeneralEngineData] engine_type=0 Engine.0=8.00, 0.00, 0.00 fuel_flow_scalar=1.00 min_throttle_limit=0.00 [Reference Speeds] flaps_up_stall_speed=79.00 full_flaps_stall_speed=63.200 cruise_speed=250.00 max_indicated_speed=760.00 [keyboard_response] elevator=350.00,500.00 aileron=450.00,1000.00 rudder=200.00,1000.00 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.00 autothrottle_available=1 pitch_takeoff_ga=8.00 max_pitch=10.00 max_pitch_acceleration=1.00 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.500 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.00 max_bank_acceleration=1.800 max_bank_velocity=3.00 max_throttle_rate=0.100 nav_proportional_control=9.00 nav_integrator_control=0.2500 nav_derivative_control=0.00 nav_integrator_boundary=2.500 nav_derivative_boundary=0.00 gs_proportional_control=9.5200 gs_integrator_control=0.2600 gs_derivative_control=0.00 gs_integrator_boundary=0.700 gs_derivative_boundary=0.00 yaw_damper_gain=0.00 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0
