[fltsim.0] title=X-35B sim=X-35B model= panel= sound= texture= kb_checklists= //ui_manufacturer=À±@/ì@ //ui_type=Lockheed X-35B JSF ui_manufacturer=Lockheed ui_type=X-35B JSF ui_variation=No.301 description=This is an aircraft that participates in the JSF plan that the United States and Britain jointly develop the attack fighter for the next term. \nX-35A(CTOL) of the conventional take-off and landing type, X-35C (CV)of the type of loading onto warship, and X-35C(STOVL) of the short field take-off vertical landing type were developed. \nX-35B was developed by repairing X-35A. \nX-35B generates the buoyancy by the shaft drive type lift fan at the center of the body in addition to the varying type engine exhaust. \nAs a result, a steadier hovering and vertical takeoff and landing are enabled. \n\nby Kazunori Ito\n KzIT16643VT@aol.com\n [General] performance=Length: 50 ft 6 in (15.37 m) \nWingspan: 35 ft 0 in (10.65 m) \nHeight: 17 ft 4 in (5.28 m) \nWing area: 459.6 ft2 (42.7 m2) \n\nEmpty weight: 26,000 lb (12,000 kg) \nLoaded weight: 44,400 lb (20,100 kg) \nMax takeoff weight: 60,000 lb (27,200 kg) \n\nPowerplant: 1~ Pratt & Whitney F135 afterburning turbofan \nDry thrust: 28,000 lbf (128 kN)[31]) \nThrust with afterburner: 43,000 lbf (191 kN w/AB) \nSecondary (High Performance), in development: 1~ General Electric/Rolls-Royce F136 afterburning turbofan, >178 kN (40,000 lbf) \nLift fan (STOVL): 1~ Rolls-Royce Lift System in conjunction with either F135 or F136 power plant, 18,000 lbf (80 kN) \n\nMaximum speed: >Mach 1.6 (1,200 mph, 1,930 km/h) \nRange: ?1,200 nm (1,400 mi, 2,200 km) on internal fuel \nRate of climb: classified (not publicly available) \nWing loading: 91.4 lb/ft2 (446 kg/m2) \nThrust/weight:\nWith full fuel: 0.968 \nWith 50% fuel: 1.22[31] \n\nCrew: 1 \n atc_type= atc_model= [WEIGHT_AND_BALANCE] reference_datum_position=0,0,0 empty_weight_CG_position=0,0,0 max_number_of_stations=50 station_load.0= 300, 10, 0, 2, station_load.1= 0, -5, -30, -6, station_load.2= 0, -5, 30, - 6, empty_weight=15000 empty_weight_roll_MOI=135000 empty_weight_pitch_MOI=262662 empty_weight_yaw_MOI=373480 empty_weight_coupled_MOI=1300 max_gross_weight=31000 [airplane_geometry] wing_area=500 wing_span=30 wing_root_chord=13.000000 wing_dihedral=-0.049438 wing_incidence=-0.494385 wing_twist=-0.999756 oswald_efficiency_factor=1.000000 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=80.000000 htail_span=20.000000 htail_pos_lon=-14.166667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=50 //140.000000 vtail_span=13.490738 vtail_sweep=0.000000 vtail_pos_lon=-14.333333 vtail_pos_vert=5.833333 elevator_area=32.0 aileron_area=11.0 rudder_area=5.0 elevator_up_limit=18 elevator_down_limit=11 aileron_up_limit=20 aileron_down_limit=15 rudder_limit=20 elevator_trim_limit=60 spoiler_limit=30 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [fuel] Center1= 0, 0, 0,400,0 LeftMain= 0, -5, 0,200,0 RightMain=0, 5, 0,200,0 External1=0,-30,-3,300,0 External2=0, 30,-3,300,0 fuel_type=2 number_of_tank_selectors=1 electric_pump=0 [contact_points] point.0=1.000, 7.417, 0.000, -7.300, 1574.803, 0.000, 0.690, 36.780, 0.657, 2.500, 1.750, 5.000, 5.000, 0.000, 0.000, 0.000 point.1=1.000, -5.217, -7.917, -7.000, 1574.803, 1.000, 0.690, 0.000, 0.439, 2.500, 0.461, 5.000, 5.000, 2.000, 0.000, 0.000 point.2=1.000, -5.217, 7.917, -7.000, 1574.803, 2.000, 0.690, 0.000, 0.439, 2.500, 0.461, 5.000, 5.000, 3.000, 0.000, 0.000 point.3 = 2, 20.584, 0.000, -1.447, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.4 = 2, -18.750, 0.000, -0.922, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.5 = -6.23, 8.43, -4.45, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.6 = -6.23, -8.43, -4.45, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.7 = 6.17, 0.00, -5.55, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 static_pitch=0.000000 static_cg_height=7.150000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=3.000000 //lift_scalar= 1.500 //none system_type=0 //1 flaps-position.0=0.000000,0.000000 flaps-position.1=1.000000,0.000000 flaps-position.2=4.000000,0.000000 flaps-position.3=8.000000,0.000000 flaps-position.4=15.000000,0.000000 flaps-position.5=27.000000,0.000000 flaps-position.6=34.000000,0.000000 [Flaps.1] type=1 span-outboard=0.500000 extending-time=3.000000 lift_scalar= 5.000 system_type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=1.000000,0.000000 flaps-position.2=2.000000,0.000000 flaps-position.3=4.000000,0.000000 flaps-position.4=80.000000,0.000000 flaps-position.5=150.000000,0.000000 [GeneralEngineData] engine_type=1 Engine.0=00.000000,0.000000,0.000000 fuel_flow_scalar=0.5 min_throttle_limit=0 max_contrail_temperature = -10 [TurbineEngineData] fuel_flow_gain=1.5 inlet_area=50 rated_N2_rpm= 27000 static_thrust=40500 afterburner_available=0 reverser_available=0 [jet_engine] thrust_scalar = 1.08 [pitot_static] vertical_speed_time_constant = 99 [Reference Speeds] flaps_up_stall_speed=1000 full_flaps_stall_speed=1000 cruise_speed=680 max_indicated_speed=1200 max_mach=1.6 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=2.0 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Views] eyepoint=14.495000,0.000000,3.245000 [Effects] [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [tailhook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=1.0 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //6=taxi light, 7=recognition light, 8=wing light, 9=logo light // Z, X, Y light.0=3, -4.99, 0.00, 3.44, fx_navred , light.1=2, -4.99, 0.00, 3.44, fx_strobe , light.2=3, -8.60, -16.83, 1.02, fx_navred , light.3=2, -8.60, -16.83, 1.02, fx_strobe , light.4=3, -8.60, -16.83, 0.49, fx_navred , light.5=2, -8.60, -16.83, 0.49, fx_strobe , light.6=3, -8.60, 16.83, 1.02, fx_navgre , light.7=2, -8.60, 16.83, 1.02, fx_strobe , light.8=3, -8.60, 16.83, 0.49, fx_navgre , light.9=2, -8.60, 16.83, 0.49, fx_strobe ,
