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Grumman XF5F Skyrocket

Military Aircraft

The Grumman XF5F Skyrocket was a prototype twin-engined shipboard fighter interceptor that the United States Navy ordered from Grumman on 30 June 1938 as the single model G-34. It had an unusual layout, with a short fuselage whose nose did not extend ahead of the wing, a twin tail, and two 1,200 horsepower Wright R-1820 radial engines driving propellers that rotated in opposite directions to cancel torque, promising high speed and an outstanding rate of climb. Provisions were included for two 20 mm cannon. It first flew on 1 April 1940 and was tested against several contemporary fighters in 1941, but the Navy settled on the Wildcat for mass production, and the prototype was struck off after a belly landing on 11 December 1944.

Facts
Year
1940 1
Engine Class
Piston 1
Top Speed (km/h)
616 1
Mass (kg)
3677 1
Maximum Mass (kg)
4944.2 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Grumman XF5F Skyrocket (Wikipedia)

Of Make

Source Grumman XF5F Skyrocket (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Grumman XF5F Skyrocket (Wikipedia)Lead sentence, manufacturer
Quote, Lead sentence, manufacturer
The United States Navy ordered one prototype, model number G-34, from Grumman Aircraft Engineering Corporation on 30 June 1938

Originated In

Also in Geography Atlas: where this subject originated.

Source Grumman XF5F Skyrocket (Wikipedia)Lead sentence, country
Quote, Lead sentence, country
The United States Navy ordered one prototype, model number G-34, from Grumman Aircraft Engineering Corporation on 30 June 1938
Sources
1. Grumman XF5F Skyrocket (Wikipedia)
  • Lead sentence
    The Grumman XF5F Skyrocket was a prototype twin-engined shipboard fighter interceptor.
  • Design and development, first flight
    The aircraft flew for the first time on 1 April 1940.
  • Specifications, powerplant
    Wright XR-1820-40/42 Cyclone nine cylinder radial air-cooled engine, 1,200 hp (895 kW) each
  • Specifications, maximum speed
    Maximum speed: 383 mph (616 km/h, 333 kn) at sea level
  • Specifications, empty weight
    Empty weight: 8,107 lb (3,600 kg)
  • Specifications, maximum takeoff weight
    Max takeoff weight: 10,900 lb (4,955 kg)
  • Lead sentence, manufacturer
    The United States Navy ordered one prototype, model number G-34, from Grumman Aircraft Engineering Corporation on 30 June 1938
  • Lead sentence, country
    The United States Navy ordered one prototype, model number G-34, from Grumman Aircraft Engineering Corporation on 30 June 1938
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