McDonnell F-101 Voodoo

· McDonnell Aircraft

Airplanes

Length

20.4216 m

Flat Wing Span

11.8872 m

Height

5.4864 m

Flat Wing Area

34.1883 m²

Max Speed

1824.996 km/h

Max Mach

1.72 Mach

Max Ceiling

17800.32 m

Number of Engines

First Flight

1954-09-29

Entry Into service

1957-05-01

Number Built

807

Maximum Take-Off Weight

23.7682 t (paragliders: kg)

Total Fuel Capacity

7771.45

Maximum Range

2446.203 km

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
McDonnell F-101 Voodoo	23.7682	7771.45	2446.203

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
McDonnell CF-101 Voodoo	Pratt & Whitney J57	20.55	12.09	Compare
Lockheed F-117 Nighthawk		19.812	13.1064	Compare
Mikoyan MiG-35		17.3	12	Compare
McDonnell Douglas CF-18 Hornet		17.0688	12.192	Compare
McDonnell Douglas F/A-18 Hornet		17.1	12.3	Compare
Vickers Type 559		20.7264	12.8016	Compare

All data (24 fields)

Name: McDonnell F-101 Voodoo
Manufacturer: McDonnell Aircraft
Description: The McDonnell F-101 Voodoo is a supersonic jet fighter designed and produced by the American McDonnell Aircraft Corporation.
First Flight: 1954-09-29
Entry Into service: 1957-05-01
Service End: 1972-01-01
Designer: McDonnell Aircraft
Type: Fighter aircraft
Length (m): 20.4216
Height (m): 5.4864
Cockpit Crew: 2
Max Speed (km/h): 1824.996
Max Ceiling (m): 17800.32
Armament: 4 (originally 6) × AIM-4 Falcon or 2 × AIR-2 Genie nuclear rockets, plus 2 × AIM-4 Falcon
Max Mach (Mach): 1.72
National Origin: Macao
Number Built: 807
Powerplant Description: 2 × Pratt & Whitney J57-P-55 afterburning turbojet engines
Primary Users: United States Air Force (historical), Republic of China Air Force (historical), Royal Canadian Air Force (historical)
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/McDonnell_F-101_Voodoo
Flat Wing Span (m): 11.8872
Flat Wing Area (m²): 34.1883
Number of Engines: 2