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Vought Corsair Junior

Military Aircraft

The Vought V-100 Corsair Junior was a cheaper, lighter and more versatile export version of the O2U and O3U Corsair observation biplanes that Vought built for the United States Navy, aimed at South American air arms with smaller budgets. It was a two-seat single-bay biplane with a 400 horsepower Pratt & Whitney Wasp Junior radial engine, a welded steel tube fuselage and wooden wings covered in fabric. Both cockpits carried flying controls so that the rear seat could serve for instrument training, or be given over to a camera, radio or gunner with a flexible machine gun, and a fixed forward gun and bomb racks could be added. The aircraft could be fitted with wheels or with a single central float. It first flew between late 1934 and early 1935, but the concept of a light multi-purpose military aircraft did not attract buyers in South America, and only the prototype was built.

Facts
Engine Class
Piston 1
Status
Prototype 1
Power (kW)
298 1
Units Built
1 1
Top Speed (km/h)
249 1
Mass (kg)
1091 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

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

Also in Business Atlas: the manufacturer of this subject.

Source Vought Corsair Junior (Wikipedia)Design and development, manufacturer
Quote, Design and development, manufacturer
Vought hoped that a smaller, lighter, more versatile and cheaper version might be successful.

Originated In

Also in Geography Atlas: where this subject originated.

Source Vought Corsair Junior (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
observation aircraft it had produced for the United States Navy
Sources
1. Vought Corsair Junior (Wikipedia)
  • Lead
    The Vought V-100 Corsair Junior was an attempt to produce a cheaper, multi-purpose, export version of the Vought O2U/O3U observation aircraft it had produced for the United States Navy.
  • Lead, status
    it did not sell and only the prototype was built.
  • Lead, units built
    it did not sell and only the prototype was built.
  • Design and development
    powered by a radial engine, a 400 hp (300 kW), nine-cylinder Pratt & Whitney Wasp Junior
  • Design and development, power
    a 400 hp (300 kW), nine-cylinder Pratt & Whitney Wasp Junior
  • Specifications
    Empty weight: 2,405 lb (1,091 kg)
  • Specifications, top speed
    Maximum speed: 155 mph (249 km/h, 135 kn)
  • Design and development, manufacturer
    Vought hoped that a smaller, lighter, more versatile and cheaper version might be successful.
  • Lead, country of origin
    observation aircraft it had produced for the United States Navy
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