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XF3W
Role Racer
National origin United States
Manufacturer Wright Aeronautical Corporation
First flight 5 May 1926[1]
Number built 1

The Wright XF3W was an American racing aircraft built by Wright Aeronautical Corporation for the US Navy.

Contents

Development and design

After the US Navy declared its preference for radial engines, Wright developed the Wright P-1 Simoon. To demonstrate the engine the F3W was designed to carry it. The F3W was a single-seat biplane, with a steel tubing fuselage and wood wings, covered by fabric. Designed to be a carrier-based fighter and powered by the Simoon engine, its performance was poor. After the Navy took delivery of the aircraft, they installed a rival companies engine, the Pratt & Whitney R-1340 radial. The aircraft was redesignated XF3W, and flew with the new engine for the first time on 5 May 1926. [1]

Operational history

The Navy used the XF3W as a test bed for the Pratt & Whitney engine until 1930, during which time the aircraft set a number of records. On 6 September 1926 the XF3W set the world altitude record for seaplanes of 38,500 ft (11,735 m). On 6 April 1930 it set the landplane altitude record of 43,166 ft (12,157 m).[1]

Specifications

Data from Angelucci, 1987. p. 462.[1]

General characteristics

  • Crew: 1
  • Length: 22 ft 1 in (6.73 m)
  • Wingspan: 27 ft 4 in (8.33 m)
  • Height: 8 ft 6 in (2.59 m)
  • Wing area: 215 ft² (19.97 m²)
  • Empty weight: 1,414 lb (641 kg)
  • Gross weight: 2,128 lb (965 kg)
  • Powerplant: 1 × Pratt & Whitney R-1340-B, 450 hp (336 kW)

Performance

  • Maximum speed: 162 mph (261 km/h)
  • Service ceiling: 38,560 ft (11,753 m)

References

  1. ^ a b c d Angelucci, 1987. p. 462.
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Bibliography

  • Angelucci, Enzo (1987). The American Fighter from 1917 to the present. New York: Orion Books. ISBN 0-517-56588-9.  

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