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U. S.
Military Aircraft Grumman XF5F SKYROCKET Photo by Coil B. Thomanel |
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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 |
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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. |