[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