[fltsim.0] title=P-59A Airacomet Clean sim=P-59A Airacomet model=C panel= sound= texture= kb_checklists= //ui_manufacturer=AJóR WFbg@ //ui_type=Bell P-59A Airacomet ui_manufacturer=Bell ui_type=P-59A Airacomet ui_variation=USAF 422610 (Clean) description=The Bell P-59A was the first United States jet fighter aircraft, designed and built during World War II. \nThe USAAF was not impressed by its performance and cancelled the contract when fewer than half of the aircraft ordered had been produced. \nAlthough no P-59s went into combat, it paved the way for another design generation of U.S. turbojet-powered aircraft and was the first turbojet fighter to have its turbojet engine and inlet nacelles integrated within the main fuselage.\n\nby Kazunori Ito\n KazuIto0926@aol.com\n [fltsim.1] title=P-59A Airacomet with Pylon sim=P-59A Airacomet model=P panel= sound= texture= kb_checklists= //ui_manufacturer=AJóR WFbg@ //ui_type=Bell P-59A Airacomet ui_manufacturer=Bell ui_type=P-59A Airacomet ui_variation=USAF 422610 (with Pylon) description=The Bell P-59A was the first United States jet fighter aircraft, designed and built during World War II. \nThe USAAF was not impressed by its performance and cancelled the contract when fewer than half of the aircraft ordered had been produced. \nAlthough no P-59s went into combat, it paved the way for another design generation of U.S. turbojet-powered aircraft and was the first turbojet fighter to have its turbojet engine and inlet nacelles integrated within the main fuselage.\n\nby Kazunori Ito\n KazuIto0926@aol.com\n [fltsim.2] title=P-59A Airacomet with Tank sim=P-59A Airacomet model=T panel= sound= texture= kb_checklists= //ui_manufacturer=AJóR WFbg@ //ui_type=Bell P-59A Airacomet ui_manufacturer=Bell ui_type=P-59A Airacomet ui_variation=USAF 422610 (with Tank) description=The Bell P-59A was the first United States jet fighter aircraft, designed and built during World War II. \nThe USAAF was not impressed by its performance and cancelled the contract when fewer than half of the aircraft ordered had been produced. \nAlthough no P-59s went into combat, it paved the way for another design generation of U.S. turbojet-powered aircraft and was the first turbojet fighter to have its turbojet engine and inlet nacelles integrated within the main fuselage.\n\nby Kazunori Ito\n KazuIto0926@aol.com\n [General] performance=Length: 38 ft 2 in (11.63 m) \nWingspan: 45 ft 6 in (13.87 m) \nHeight: 12 ft 4 in (3.76 m) \nWing area: 386 ft2 (35.9 m2) \n\nEmpty weight: 7,940 lb (3,600 kg) \nMax takeoff weight: 12,700 lb (5,760 kg) \n\nPowerplant: 2~ General Electric I-A turbojets, 2,000 lbf (8.9 kN) each \n\nMaximum speed: 413 mph (664 km\/h) \nRange: 240 mi (386 km) \nService ceiling 46,200 ft (14,080 m) \nRate of climb: 3,200 ft\/min (16,26 m\/s) \n\nArmament:1x 37 mm cannon \n 3x .50 cal (12.7 mm) machine guns \n\nCrew: 1 \n atc_type= atc_model= [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=7600.000000 empty_weight_roll_MOI=28000.000000 empty_weight_pitch_MOI=48000.000000 empty_weight_yaw_MOI=24000.000000 empty_weight_coupled_MOI=1300.000000 [airplane_geometry] wing_area=200.000000 wing_span=30.500000 wing_root_chord=7.333333 wing_dihedral=0.000000 wing_incidence=-0.494385 wing_twist=0.000000 oswald_efficiency_factor=1.871080 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=47.000000 htail_span=14.166667 htail_pos_lon=-16.333333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=40.000000 vtail_span=7.211103 vtail_sweep=0.000000 vtail_pos_lon=-16.333333 vtail_pos_vert=5.833333 elevator_area=7.500000 aileron_area=6.880000 rudder_area=3.400000 elevator_up_limit=28.647890 elevator_down_limit=28.647890 aileron_up_limit=17.761692 aileron_down_limit=17.761692 rudder_limit=22.918312 elevator_trim_limit=19.480565 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [fuel] Center1=0.000000,0.000000,0.000000,68.000000,0.000000 LeftMain=0.000000,0.000000,0.000000,74.000000,0.000000 LeftAux=0.000000,-5.000000,0.000000,35.000000,0.000000 LeftTip=0.000000,-10.000000,0.000000,26.000000,0.000000 RightMain=0.000000,0.000000,0.000000,74.000000,0.000000 RightAux=0.000000,5.000000,0.000000,35.000000,0.000000 RightTip=0.000000,10.000000,0.000000,26.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [contact_points] point.0=1.000000, 16.404000, 0.000000,-4.80000, 2776.282603, 0.000000, 0.574715, 39.000000, 0.107873, 1.500000, 0.317230, 5.000000, 5.000000, 0.000000,0.000000,0.000000 point.1=1.000000, -3.55000,-5.083333,-4.900000, 2776.282603, 1.000000, 0.574715, 0.000000, 0.390256, 2.500000, 0.577863, 5.000000, 5.000000, 2.000000,0.000000,0.000000 point.2=1.000000, -3.515000, 5.083333,-4.900000, 2776.282603, 2.000000, 0.574715, 0.000000, 0.390256, 2.500000, 0.577863, 5.000000, 5.000000, 3.000000,0.000000,0.000000 point.3=2.000000, 0.000000,-15.583333,0.666667,1574.803150,0.000000,0.000000, 0.000000, 0.000000, 0.000000,0.000000, 0.000000, 0.000000, 5.000000,0.000000,0.000000 point.4=2.000000, 0.000000, 15.583333,0.666667,1574.803150,0.000000,0.000000, 0.000000, 0.000000, 0.000000,0.000000, 0.000000, 0.000000, 6.000000,0.000000,0.000000 point.5=2.000000, -15.666667, 0.000000,-0.166667,1574.803150,0.000000,0.000000, 0.000000, 0.000000, 0.000000,0.000000, 0.000000, 0.000000, 9.000000,0.000000,0.000000 point.6=2.000000, 8.000000, 0.000000,-0.166667,1574.803150,0.000000,0.000000, 0.000000, 0.000000, 0.000000,0.000000, 0.000000, 0.000000, 4.000000,0.000000,0.000000 static_pitch=0.000000 static_cg_height=4.85 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=19.999092,0.000000 flaps-position.2=39.998184,0.000000 [GeneralEngineData] engine_type=1 Engine.0=-6.000000,-1.180000,0.000000 Engine.1=-6.000000,1.180000,0.000000 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=4.471680 rated_N2_rpm=29920.000000 static_thrust=2100.000000 afterburner_available=0 reverser_available=0 [Reference Speeds] flaps_up_stall_speed=82.000000 full_flaps_stall_speed=65.600000 cruise_speed=456.372410 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=6.191000, 0.000000, 2.208000 [direction_indicators] direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [LIGHTS] light.0=3, 4.04, 22.90, 1.08, fx_navgre , light.1=3, 4.04, -22.90, 1.08, fx_navred , light.2=3, -1.57, 0.00, 2.53, fx_navred ,
