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U. S. Military Aircraft

Grumman XF5F SKYROCKET

Photo by Coil B. Thomanel

In 1938 Grumman proposed a naval interceptor with two engines. Such a power plant was a completely new feature for shipboard aircraft, and the G-34 was also revolutionary in its configuration. This located the wing leading edge forward of the fuselage's stubby nose. The layout was completed by a high set cockpit, counter rotating propellers, rearward retracting main units foe the tail wheel landing gear, and a dihedralled tail plane with endplate vertical suffices. The US. Navy order a single XF5F-1 in June 1938, and this first flew in April 1940. The type was extensively tested, and nose was later extended to a point forward of the leading edge. No production was order, but by the time it was retired in December 1944 the plane had contributed to the F7Fs development. The G-46 version with a more conventional fuselage and tricycle landing gear interested the US. Army Air Force which order a single XP-50 prototype. The first flew in May 1941, and reached 424 mph. at 25,000 ft. The type suffered constant problems with its power plant of two R-1820-67/69 radials and was finally written off after the explosion of the turbocharger. 

 

 

TECHNICAL DATA

Description Specifications
Manufacturer: Grumman Length: 28 ft. 8.5 in.
First Flight: XF5F-1 April, 1940. XF-50 May, 1941 Height: 11 ft. 4 in.
Model:  Wing Span: 42 ft. 0 in.
Crew: One Wing Area: 303.5 sq. in.
Nickname: Skyrocket Empty Weight: 8,107 lb.
Basic Role: Carrierborne Interceptor Max. Weight: 10,138 lb.
Other Versions: XF5F-1 naval prototype.
XP-50 land base prototype.
Armament: Four 0.5-in 12.7-mm machine guns.
Principal User: USA

Propulsion

Performance

Power Plant: Wright R-1820-40/42 Cyclone radial piston engines.
Range: 1,200 miles. Horsepower: 1,200-hp.
Max. 383 mph. No. Of Engines: Two  
Ceiling: 33,000 ft.  
Climb Rate: 4,000 ft. per minute.  

 

 

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