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
Engine Class Engine Class Top Speed (km/h) Maximum Mass (kg) EngineWestinghouse J34 turbojet 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source McDonnell XF-88 Voodoo (Wikipedia)
Of Make
Source McDonnell XF-88 Voodoo (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source McDonnell XF-88 Voodoo (Wikipedia)Design and developmentQuote, 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 originQuote, 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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