[fltsim.0] title=F-101B NDANG sim=F-101 model= panel= sound= texture=NDANG kb_checklists= atc_id=70297 atc_airline=NODAK atc_flight_number=297 ui_manufacturer=McDONNELL DOUGLAS ui_type=F-101B VooDoo ui_variation=North Dakota ANG description=The F-101B was a two-seat all-weather interceptor variant of the Voodoo, and was numerically the most important Voodoo variant, with a total of 479 being built. The first F-101Bs were delivered to the 60th Interceptor Squadron at Otis AFB in Massachusetts on January 5, 1959. F-101Bs began to leave active duty with the USAF beginning in 1969, many aircraft being passed along to the Air National Guard. The first F-101Bs were delivered to the Air National Guard in November of 1969, entering service with the 116th Fighter Interceptor Squadron of the Washington ANG and the 132nd FIS of the Maine ANG. They also served with the 179th FIS of the Minnesota ANG, the 136th FIS of the New York ANG, the 137th FIS of the New York ANG, the 192nd FIS of the Nevada ANG, the 178th FIS of the North Dakota ANG, the 123rd FIS of the Oregon ANG, and the 111th FIS of the Texas ANG. The F-101B passed out of ANG service when the last F-101B was retired by the 111th FIS in 1981. [General] atc_type=MCDONNELL DOUGLAS atc_model=F101 performance=Engines: Two Pratt & Whitney J57-P-55 turbojets, 11,990 lb.s.t. dry and 16,900 lb.s.t. with afterburner. Dimensions: wingspan 39 feet 8 inches, length 67 feet 5 inches, height 18 feet 0 inches, wing area 368 square feet. Performance: Maximum speed 1134 mph at 35,000 feet (Mach 1.72). Initial climb rate 49,200 feet/min. Service ceiling 58,400 feet, combat ceiling 51,000 feet. Normal range 1520 miles, maximum range 1930 miles. Weights: 28,970 pounds empty, 45,664 pounds gross, 40,853 pounds combat weight, 52,400 pounds maximum takeoff. Fuel: Maximum internal fuel load was 2053 US gallons. A total of two 450 US gallon under-fuselage drop tanks could be carried, bringing maximum fuel load to 2953 US gallons. Armament: Armed with four Falcon AAMs (usually 2 GAR-1 (AIM-4) semiactive radar homers and 2 GAR-2 (AIM-4B) infrared homers) in an internal ventral weapons bay. In later versions, two unguided AIR-2A Genie unguided rockets with nuclear warheads could be carried in place of two of the Falcons. [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=32353.000000 empty_weight_roll_MOI=288625.000000 empty_weight_pitch_MOI=300000.000000 empty_weight_yaw_MOI=300000.000000 empty_weight_coupled_MOI=1300.000000 max_gross_weight=48529.500000 [fuel] LeftMain=0.000000,0.000000,0.000000,914.000000,0.000000 LeftAux=0.000000,-15.333333,0.000000,300.000000,0.000000 RightMain=0.000000,0.000000,0.000000,914.000000,0.000000 RightAux=0.000000,15.333333,0.000000,300.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=531.000000 wing_span=38.416667 wing_root_chord=13.833333 wing_dihedral=2.999268 wing_incidence=-0.494385 wing_twist=-0.999756 oswald_efficiency_factor=7.498099 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=96.000000 htail_span=16.416667 htail_pos_lon=-24.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=67.000000 vtail_span=9.332738 vtail_sweep=0.000000 vtail_pos_lon=-19.666667 vtail_pos_vert=5.833333 elevator_area=24.000000 aileron_area=21.240000 rudder_area=11.390000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 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 [contact_points] point.0=1.000000,22.166667,0.000000,-4.916667,1574.803150,0.000000,0.837058,45.960000,0.297617,2.500000,0.649818,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-1.666667,-8.916667,-4.916667,1574.803150,1.000000,0.837058,0.000000,0.297619,2.500000,0.649836,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-1.666667,8.916667,-4.916667,1574.803150,2.000000,0.837058,0.000000,0.297619,2.500000,0.649836,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2.000000,-6.916667,-19.083333,1.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-6.916667,19.083333,1.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-26.166667,0.083333,5.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,22.166667,0.000000,5.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.000000 static_cg_height=4.917881 gear_system_type=0 [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=13.330818,0.000000 flaps-position.2=26.661636,0.000000 flaps-position.3=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=-4.333333,-2.083333,1.083333 Engine.1=-4.333333,2.083333,1.083333 fuel_flow_scalar=1.000000 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=21.519960 rated_N2_rpm=29920.000000 static_thrust=17933.300000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=129.000000 full_flaps_stall_speed=103.200000 cruise_speed=743.286401 max_indicated_speed=1593.750000 max_mach=2.399902 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=19.902908,0.000000,4.805918 [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 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [direction_indicators] direction_indicator.0=3,0 [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, 8.04, 0.00, 6.43, fx_navred , light.1=2, 8.04, 0.00, 6.43, fx_strobe , light.2=3, 1.61, 0.00, -1.54, fx_navred , light.3=2, 1.61, 0.00, -1.54, fx_strobe , light.4=3, -9.45, 20.51, 0.52, fx_navgre , light.5=2, -9.45, 20.51, 0.52, fx_strobe , light.6=3, -9.45, -20.51, 0.52, fx_navred , light.7=2, -9.45, -20.51, 0.52, fx_strobe , light.8=3, -34.35, 0.00, 13.25, fx_navwhi , //fx_efaburner = normal point + 3.76 light.9=6, -20.28, 2.00, 4.45, fx_efaburner light.10=6, -20.28, -2.00, 4.45, fx_efaburner [brakes] toe_brakes_scale=1.000031 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0