Vought XF3U

From Wikipedia, the free encyclopedia
Jump to: navigation, search
XF3U
Role Fighter
National origin United States
Manufacturer Vought
First flight May 9, 1933[1]
Number built 1
Developed into SBU Corsair

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.

[edit] Development and design

The XF3U was designed to meed 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. Of the seven proposed aircraft the XF3U and the Douglas XFD were chosen. The XF3U was the first all-metal aircraft produced by Vought. The aircraft was also equipped with an enclosed cockpit. During flight testing in 1933, it outperformed the Douglas entry and was chosen the winner.

[edit] Operational history

The Navy no longer was interested in two-seat fighters, and therefore only the one XF3U prototype aircraft was built. The XF3U subsequently evolved into a dive bomber, and became the XSBU prototype for the SBU-1 Corsair.[1]


[edit] Specifications

Data from [1]

General characteristics

Performance

Armament

3 × .30 in (7.62 mm) machine guns

[edit] References

Notes
  1. ^ a b c Angelucci 1987, p. 434.
Bibliography
  • Angelucci,Enzo. The American Fighter from 1917 to the present. New York: Orion Books, 1987. ISBN 0-517-56588-9.