[fltsim.0] title=CURTISS HAWK P36 NL sim=HAWK_P36 model= panel= sound= texture= KB_checklists=CURTISS HAWK P36 description=The Curtiss P-36 Hawk, also know as Curtiss \nHawk Model 75,was a U.S.-built fighter aircraft \nof the 1930s. A contemporary of the Hawker \nHurricane and Messerschmitt Bf 109, it was one \nof the first fighters of the new generation sleek \nmonoplanes with extensive use of metal in \nconstruction and powerful piston engines, was \nextensively used by the French Air Force and \nalso by British Commonwealth and Chinese\n ui_manufacturer=Curtiss UI_VARIATION=DUTCH [fltsim.1] title=CURTISS HAWK P36 USAAC sim=HAWK_P36 model= panel= sound= texture=US KB_checklists=CURTISS HAWK P36 description=The Curtiss P-36 Hawk, also know as Curtiss \nHawk Model 75,was a U.S.-built fighter aircraft \nof the 1930s. A contemporary of the Hawker \nHurricane and Messerschmitt Bf 109, it was one \nof the first fighters of the new generation sleek \nmonoplanes with extensive use of metal in \nconstruction and powerful piston engines, was \nextensively used by the French Air Force and \nalso by British Commonwealth and Chinese\n ui_manufacturer=Curtiss UI_VARIATION=USAAC [fltsim.2] title=CURTISS HAWK P36 NATIONAL CHINA sim=HAWK_P36 model= panel= sound= texture=SI KB_checklists=CURTISS HAWK P36 description=The Curtiss P-36 Hawk, also know as Curtiss \nHawk Model 75,was a U.S.-built fighter aircraft \nof the 1930s. A contemporary of the Hawker \nHurricane and Messerschmitt Bf 109, it was one \nof the first fighters of the new generation sleek \nmonoplanes with extensive use of metal in \nconstruction and powerful piston engines, was \nextensively used by the French Air Force and \nalso by British Commonwealth and Chinese\n ui_manufacturer=Curtiss UI_VARIATION=NATIONALIST CHINA [General] editable=0 atc_type= atc_model= performance=Crew: One \nLength: 28 ft 6 in (8.7 m) \nWingspan: 37 ft 1 in (11.3 m) \nHeight: 9 ft 2 in (2.8 m) \nWing area: 235.6 ft² (21.9 m²) \nEmpty weight: 4,665 lb (2,116 kg) \nLoaded weight: 5,867 lb (2,661 kg) \nMax takeoff weight: lb (kg) \nPowerplant: 1× Pratt & Whitney R-1830-13 Twin Wasp air-cooled radial piston engine, 1,050 hp (783 kW) \nPerformance\nMaximum speed: 322 mph (518 km\/h) \nCruise speed: 260 mph (420 km\/h) \nRange: 650 mi (1,046 km) \nService ceiling: 32,340 ft (9,860 m) \nRate of climb: 2,500 [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 [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=2700.000000 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 [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 [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, -16.80, 0.00, -0.75, 3200, 0, 0.40,180.0, 0.30, 2.5, 0.90, 3.0, 3.0, 0, 0, 235 point.1=1, 1.40, -3.91, -4.65, 2200, 1, 1.13, 0.0, 0.45, 2.5, 0.83, 4.5, 4.5, 2, 0, 235 point.2=1, 1.40, 3.91, -4.65, 2200, 2, 1.13, 0.0, 0.45, 2.5, 0.83, 4.5, 4.5, 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, -16.25, 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=5.85 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch=10.69 //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=40 // degrees, KIAS damaging-speed=201 // KIAS blowout-speed=305 // KIAS [LIGHTS] 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
