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Vought O4U Corsair

Military Aircraft

The Vought O4U Corsair was the designation applied to two different experimental biplane scout-observation aircraft, neither of which reached production or entered regular service. The United States Navy ordered the type in 1930 as the third of its lightweight observation designs, alongside the Keystone XOK-1 and the Berliner-Joyce XOJ-1. The XO4U-1, built in 1931, was Vought's first airplane with a deep monocoque two-place fuselage and had a metal and fabric covered metal wing structure, powered by a 500 horsepower Pratt & Whitney R-1340D Wasp radial. It first flew in February 1931 and crashed on 28 February when test pilot Carl Harper could not recover from a spin and had to parachute out. The second airframe, the XO4U-2, was in effect an O3U-3 Corsair with a cowled Twin Wasp Junior engine that first flew in June 1932 and was tested in the NACA full scale wind tunnel at Langley in 1933.

Facts
Year
1931 1
Engine Class
Piston 1
Status
Prototype 1
Power (kW)
373 1
Top Speed (km/h)
230 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Vought O4U Corsair (Wikipedia)
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Manufactured By

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Source Vought O4U Corsair (Wikipedia)Design and development, manufacturer
Quote, Design and development, manufacturer
The Vought XO4U-1, BuNo A-8641, was built in 1931, and was Vought's first airplane with a deep monocoque two-place fuselage

Originated In

Also in Geography Atlas: where this subject originated.

Source Vought O4U Corsair (Wikipedia)Design and development, country of origin
Quote, Design and development, country of origin
Ordered by the United States Navy in 1930 as the third type of "lightweight" observation aircraft designs
Sources
1. Vought O4U Corsair (Wikipedia)
  • Lead
    The Vought O4U Corsair was the designation applied to two different experimental biplane scout-observation aircraft.
  • Lead, status
    Neither reached production or entered regular service.
  • Operational history
    The sole XO4U-1 first flew in February 1931, but crashed on 28 February 1931
  • Design and development
    Powered by a 500 hp (370 kW) Pratt & Whitney R-1340D Wasp 9-cylinder air-cooled radial engine driving a two-bladed fixed-pitch propeller.
  • Design and development, power
    Powered by a 500 hp (370 kW) Pratt & Whitney R-1340D Wasp 9-cylinder air-cooled radial engine
  • Specifications
    Maximum speed: 143 mph (230 km/h, 124 kn)
  • Design and development, manufacturer
    The Vought XO4U-1, BuNo A-8641, was built in 1931, and was Vought's first airplane with a deep monocoque two-place fuselage
  • Design and development, country of origin
    Ordered by the United States Navy in 1930 as the third type of "lightweight" observation aircraft designs
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