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McDonnell XF-88 Voodoo

Military Aircraft

The McDonnell XF-88 Voodoo was a long-range twin-jet fighter that McDonnell Aircraft built as a prototype for the United States Air Force in the late 1940s. It grew out of a 1946 requirement for a penetration fighter able to escort bombers to their targets, a jet replacement for the wartime P-51 Mustang in that role. Two prototypes were ordered, the first flew on 20 October 1948, and the second was fitted with afterburners to cure the underpowered first design. The type won the Air Force penetration fighter competition against the Lockheed XF-90 and North American YF-93, but the requirement was cancelled in August 1950 and it never entered production. One prototype was later rebuilt as the XF-88B propeller research aircraft, the first propeller-equipped aircraft to exceed Mach 1. Its layout, with swept wings and engines in the lower fuselage, was enlarged into the supersonic F-101 Voodoo.

Facts
Year
1948 1
Engine Class
Jet 1
Engine Class
Turboprop 1
Status
Cancelled 1
Status
Scrapped 1
Units Built
2 1
Top Speed (km/h)
1136 1
Mass (kg)
5507 1
Maximum Mass (kg)
10,478 1
Engine
Westinghouse J34 turbojet 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source McDonnell XF-88 Voodoo (Wikipedia)

Of Make

Source McDonnell XF-88 Voodoo (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source McDonnell XF-88 Voodoo (Wikipedia)Design and development
Quote, Design and development
McDonnell began work on the aircraft, dubbed Model 36, on 1 April 1946.

Originated In

Also in Geography Atlas: where this subject originated.

Source McDonnell XF-88 Voodoo (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
designed for the United States Air Force
Sources
1. McDonnell XF-88 Voodoo (Wikipedia)
  • Operational history, first flight
    The first XF-88 made its maiden flight from Muroc Field on 20 October 1948
  • Operational history, cancellation
    led the penetration fighter to be cancelled in August 1950
  • Operational history, fate
    Both prototypes were scrapped by 1958.
  • Lead
    was a long-range, twinjet fighter aircraft designed for the United States Air Force
  • Design and development, engines
    specified as Westinghouse J34 turbojets
  • Operational history, XF-88B
    nose-mounted Allison T38 turboprop
  • Specifications (XF-88A), empty weight
    Empty weight: 12,140 lb (5,507 kg)
  • Specifications (XF-88A), max takeoff weight
    Max takeoff weight: 23,100 lb (10,478 kg)
  • Specifications (XF-88A), maximum speed
    Maximum speed: 706 mph (1,136 km/h, 613 kn)
  • Design and development, contract
    the company was given a contract for two prototypes designated XP-88
  • Design and development
    McDonnell began work on the aircraft, dubbed Model 36, on 1 April 1946.
  • Lead, country of origin
    designed for the United States Air Force
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