| Early in 1927, the US Navy BuAer conceived a requirement
for a two-seat fighter for fleet defence and
contracts were signed on 30 June for the XF2U-1 and
the Curtiss XF8C-2. As it was found that the fighter could not be based, as at first hoped, on the O2U observation
aircraft, considerable delay resulted in completing
the Vought prototype, which was not flown until 21
June 1929. The XF2U-1 had a steel-tube fuselage,
wooden wings and fabric skinning, power being supplied
by a 450hp Pratt & Whitney R-1340C Wasp
engine and armament comprising two 7.62mm
machine guns in the upper wing centre section and a
similar calibre weapon on a flexible mount in the rear
cockpit. By the time that the XF2U-1 reached Anacostia
for official evaluation, the BuAer had already placed a
contract for further development of the competitive
Curtiss fighter (XF8C-4), and although the Vought aircraft
met all contractual guarantees it was rejected.
Assigned to the Naval Aircraft Factory in February 1930
as a utility aircraft, it was damaged beyond repair on 6
March 1931.
 | A three-view drawing (1280 x 948) |
WEIGHTS |
Take-off weight | 1763 kg | 3887 lb |
Empty weight | 1148 kg | 2531 lb |
DIMENSIONS |
Wingspan | 10.97 m | 36 ft 0 in |
Length | 8.23 m | 27 ft 0 in |
Height | 305 m | 1001 ft 8 in |
PERFORMANCE |
Max. speed | 235 km/h | 146 mph |
Range | 797 km | 495 miles |
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