The Vought XF3U was the prototype of a two-seat, all-metal biplane fighter built by Vought at Dallas, Texas for the United States Navy. It was designed to Bureau of Aeronautics Design Specification No. 111 of 1932, which called for a high-performance fighter with a fixed undercarriage and a Pratt & Whitney R-1535 Twin Wasp Junior radial engine. Of seven proposals, the Berliner-Joyce XF3J-1, Curtiss XF12C-1, Chance Vought XF3U-1 and Douglas XFD-1 were chosen, and prototypes were ordered on 30 June 1932. The XF3U was the first all-metal aircraft Vought produced and had an enclosed cockpit. In flight testing in 1933 it outperformed the Douglas entry and was chosen the winner, but the Navy had lost interest in two-seat fighters and only the one prototype, Bureau number 9222, was built. The design then evolved into a dive bomber, the XSBU prototype for the SBU-1 Corsair, and the aircraft was also redesignated the XSBU.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Vought XF3U (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
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The Vought XF3U was the prototype of a two-seat, all-metal biplane fighter, built by Vought Aircraft Company of Dallas, Texas for the United States Navy.
Originated In
Also in Geography Atlas: where this subject originated.
Source Vought XF3U (Wikipedia)Lead, country of originQuote, Lead, country of origin
built by Vought Aircraft Company of Dallas, Texas for the United States Navy
Sources
1. Vought XF3U (Wikipedia)
Lead
The Vought XF3U was the prototype of a two-seat, all-metal biplane fighter, built by Vought Aircraft Company of Dallas, Texas for the United States Navy.
Development and design
During flight testing in 1933, it outperformed the Douglas entry and was chosen the winner.
Operational history
therefore only the one XF3U prototype aircraft was built.
Development and design, engine class
The XF3U was designed to meet the Bureau of Aeronautics 1932 Design Specification No. 111, which called for a high-performance fighter with a fixed undercarriage and powered by a Pratt & Whitney R-1535 Twin Wasp Junior air-cooled radial engine.
Specifications
Empty weight: 3,435 lb (1,558 kg)
Specifications, maximum mass
Max takeoff weight: 5,297 lb (2,402 kg)
Specifications, top speed
Maximum speed: 208 mph (334 km/h, 181 kn)
Lead, country of origin
built by Vought Aircraft Company of Dallas, Texas for the United States Navy
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