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Grumman XF5F Skyrocket

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XF5F Skyrocket
Role

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Manufacturer

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First flight

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This page is a soft redirect. 1 April 1940 #REDIRECTmw:Help:Magic words#Other
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Retired

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This page is a soft redirect. 11 December 1944 #REDIRECTmw:Help:Magic words#Other
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Number built

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Variants

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The Grumman XF5F Skyrocket was a prototype twin-engined shipboard fighter interceptor. The U. S. Navy ordered one prototype, model number G-34, from Grumman Aircraft Engineering Corporation on 30 June 1938; its designation was XF5F-1. The aircraft had a unique appearance: The forward "nose" of the fuselage did not extend forward of the wing. Provisions were included for two 23 mm (0.91 in) Madsen cannon as armament.

Design and development

In 1938 Grumman presented a proposal to the U. S. Navy for a twin engine carrier based aircraft, unlike any other fighter aircraft that had ever been considered. The design was for a light weight fighter (under 10,000 lbs maximum takeoff weight) powered by two 1,200 hp Wright R-1820 engines, with propellers geared to rotate in opposite directions to cancel out the effects of each engine's torque, promising high-speed and an outstanding rate of climb.[1]

The XF5F Skyrocket was a low wing monoplane with a short fuselage that began aft of the wing's leading edge with a twin tail assembly that featured a pronounced dihedral to the horizontal stabilizer. The main landing gear and tail wheel were fully retractable.[2]

File:Grumman XF5F-1 Skyrocket.jpg
Grumman XF5F-1 Skyrocket c. 1940

Operational history

The aircraft flew for the first time on 1 April 1940. Engine cooling problems arose in the initial flights, resulting in modification to the oil cooling ducts. Further modifications were made to the prototype including reduction in the height of the cockpit canopy, revising the armament installation to four 0.5 in (12.7 mm) machine guns in place of the cannon, redesign of the engine nacelles, adding spinners to the propellers, and extending the fuselage forward of the wing. These changes were completed on 15 July 1941.

Testing by Grumman test pilot "Connie" Converse indicated "the flying qualities for the XF5F-1 were good overall. The counter-rotating props were a nice feature, virtually eliminating the torque effect on takeoff ... single-engine performance was good, rudder forces tended to be high in single engine configuration. Spin recovery was positive but elevator forces required for recovery were unusually high. All acrobatics were easily performed, and of course forward visibility was excellent."[3] In 1941, Navy pilots tested the XF5F-1 in a fly-off against the Supermarine Spitfire, Hawker Hurricane, Curtiss P-40 Warhawk, Bell P-39 Airacobra, Bell XFL Airabonita, Vought XF4U Corsair, Grumman F4F Wildcat, and Brewster F2A Buffalo.[4]

LCDR Crommelin, in charge of the test, stated in a 1985 letter to George Skurla, Grumman president, "for instance, I remember testing the XF5F against the XF4U on climb to the 10,000 foot level. I pulled away from the Corsair so fast I thought he was having engine trouble. The F5F was a carrier pilot's dream, as opposite rotating propellers eliminated all torque and you had no large engine up front to look around to see the LSO (landing signal officer) ... The analysis of all the data definitely favored the F5F, and the Spitfire came in a distant second. ... ADM Towers told me that securing spare parts ... and other particulars which compounded the difficulty of building the twin-engine fighter, had ruled out the Skyrocket and that the Bureau had settled on the Wildcat for mass production."[4]

Additional changes were needed after further flight tests that were not completed until 15 January 1942. In the meantime, Grumman began work on a more advanced twin-engine shipboard fighter, the XF7F-1, and further testing with the XF5F-1 supported the development of the newer design. The prototype continued to be used in various tests, although plagued by various landing gear problems, until it was struck from the list of active aircraft after it made a belly landing on 11 December 1944.

Specifications (XF5F Skyrocket)

General characteristics

Performance

  • Maximum speed: 383 mph at sea level (616 km/h)
  • Range: 1,200 mi (1,800 km)
  • Service ceiling: 33,000 ft (11,000 m)
  • Rate of climb: 4,000 ft/min (1,220 m/min)</ul>Armament
  • 2 × 0.5 in (12.7 mm) machine guns
  • 2 x 0.3 in (7.62mm) machine guns
  • 2 × Script error: No such module "convert". bombs

Notable appearances in media

The XF5F Skyrocket was the only propeller fighter aircraft flown by the Blackhawks in Quality Comics monthly title Military Comics, which ran throughout World War II. The XF5F remained the Blackhawk Squadron's mount until their conversion to jet aircraft in Quality's retitled Modern Comics at the start of the jet age.[5]

See also

Related development
Aircraft of comparable role, configuration and era

References

Notes

  1. ^ "The 'Fastest Pursuit' Grumman Skyrocket XF5F/Black Hawk." fiddlersgreen.net, 2012. Retrieved: 18 May 2012.
  2. ^ Thompson, Dan. "Grumman F5F-1 Skyrocket." Blackhawk, 2012. Retrieved: 18 May 2012.
  3. ^ Lucabaugh and Martin 1995, p. 14.
  4. ^ a b Lucabaugh and Martin 1995, p. 16.
  5. ^ Greenberger 2008, p. 54.

Bibliography

  • Green, William. War Planes of the Second World War, Volume Four: Fighters. London: Macdonald & Co.(Publishers), 1961. ISBN 0-356-01448-7.
  • Green, William and Gordon Swanborough. WW2 Aircraft Fact Files: US Navy and Marine Corps Fighters. London, UK: Macdonald and Jane's, 1976. ISBN 0-356-08222-9.
  • Greenberger, Robert. "Blackhawk". In Dougall, Alastair. The DC Comics Encyclopedia. London: Dorling Kindersley, 2008. ISBN 0-7566-4119-5.
  • Lucabaugh, David and Bob Martin. Grumman XF5F-1 & XP-50 Skyrocket, Naval fighters number thirty-one. Simi Valley, California: Ginter Books, 1995. ISBN 0-942612-31-0.
  • Morgan, Eric B. "Grumman F7F Tigercat F.7/30". Twentyfirst Profile, Volume 1, No. 11. New Milton, Hants, UK: 21st Profile Ltd. ISSN 0961-8120.
  • Morgan, Eric B. "The Grumman Twins". Twentyfirst Profile, Volume 2, No. 15. New Milton, Hants, UK: 21st Profile Ltd. ISSN 0961-8120.
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