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
Engine Class Top Speed (km/h) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Vought O4U Corsair (Wikipedia)
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Manufactured By
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Source Vought O4U Corsair (Wikipedia)Design and development, manufacturerQuote, 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
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Source Vought O4U Corsair (Wikipedia)Design and development, country of originQuote, 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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