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<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->{{Infobox Aircraft |
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{|{{Infobox Aircraft Begin |
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|name = XF14C |
|name = XF14C |
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|image = File:Curtiss XF14C-2.jpg |
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|type = Carrier fighter |
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|manufacturer = [[Curtiss-Wright Corporation|Curtiss]] |
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|image = |
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|caption = |
|caption = |
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}}{{Infobox Aircraft Type |
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|type = Carrier-based fighter |
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|national origin = [[United States]] |
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|manufacturer = [[Curtiss-Wright]] |
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|designer = |
|designer = |
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|first flight = July |
|first flight = July 1944 |
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|introduced = |
|introduced = |
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|retired = |
|retired = |
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|status = |
|status = Canceled |
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|primary user = [[United States Navy|US Navy]] |
|primary user = [[United States Navy|US Navy]] |
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|more users = |
|more users = |
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|variants with their own articles = |
|variants with their own articles = |
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The '''Curtiss XF14C''' was an airplane developed by the [[Curtiss-Wright Corporation]] in response to a request by the [[U.S. Navy]] in 1941 to produce a new shipboard high-performance [[fighter aircraft]] powered by the [[Lycoming XH-2470]] [[liquid-cooled engine]]. On [[June 30]] [[1941]] a contract for two [[prototype]] aircraft, designated the '''XF14C-1''', was awarded. On the same date prototype development contracts were also awarded to [[Grumman Aircraft Engineering Corporation]] for the single engine [[XF6F-1]] and the twin engine [[XF7F-1]]. |
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The '''Curtiss XF14C''' was an American naval [[fighter aircraft]]. It was developed by [[Curtiss-Wright]] in response to a request by the [[United States Navy]] in 1941 to produce a new [[Aircraft carrier|shipboard]] high-performance fighter aircraft. |
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Early in the development the Navy requested better altitude performance and, in view of unsatisfactory progress in the development of the XH-2470 engine, Curtiss adapted the design of the aircraft around the new [[turbocharged]] [[Wright R-3350]] Duplex-Cyclone engine. The aircraft equipped with this eighteen cylinder twin row [[radial engine|radial]] [[air-cooled engine]] and three bladed [[contra-rotating propellers]] was designated the '''XF14C-2'''. The XF14C-1 was canceled. Also, looking at the problems of operation at altitudes of about 40,000 feet (12,000 m), the Navy also initiated work on a third version with a pressurized [[cockpit]] designated the '''XF14C-3'''. |
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==Design and development== |
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Ultimately, only the XF14C-2 prototype was completed, flying for the first time in July [[1944]]. Moreover, disappointment with performance estimates and delays with the availability of the XR-3350-16 engine coupled with the tactical need for an extremely high altitude fighter that failed to materialize led to cancellation of the development. |
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In 1941 the US Navy requested a better-performing carrier-based fighter plane, to be powered by the proposed [[Hyper engine|high performance]] 24-cylinder liquid cooled [[Lycoming H-2470|Lycoming XH-2470 Hyper engine]]. This was an unusual step for the Navy, which had been adamant to that time that all its aircraft use air-cooled radial engines. |
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On June 30, 1941 a contract for two [[prototype]] aircraft, designated the '''XF14C-1''', was awarded to the Curtiss-Wright company. On the same date prototype development contracts were also awarded to [[Grumman Aircraft Engineering Corporation]] for the single-engine [[Grumman Hellcat|XF6F-1]] and the twin engine [[Grumman Tigercat|XF7F-1]], both of which would use air-cooled [[Pratt & Whitney R-2800 Double Wasp]] radial engines. |
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Early in the development the Navy requested better altitude performance and, in view of unsatisfactory progress in the development of the XH-2470 engine, Curtiss adapted the design of the aircraft around the new [[turbocharged]] [[Wright R-3350]] Duplex-Cyclone air-cooled radial engine. The aircraft equipped with this eighteen-cylinder twin-row [[radial engine|radial]] [[air-cooled engine]] and three bladed [[contra-rotating propellers]] was designated the '''XF14C-2'''. The XF14C-1 was canceled. Also, looking at the problems of operation at altitudes of about 40,000 feet (12,000 m), the Navy also initiated work on a third version with a [[Pressurized cabin|pressurized cockpit]] designated the '''XF14C-3'''. |
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Ultimately, only the XF14C-2 prototype was completed, flying for the first time in July 1944. Moreover, disappointment with performance estimates and delays with the availability of the XR-3350-16 engine coupled with the evaporating tactical need for an extremely high-altitude fighter led to cancellation of the development. |
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==Specifications (XF14C-2)== |
==Specifications (XF14C-2)== |
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{{Aircraft specs |
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{{aircraft specifications |
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|ref=Curtiss Aircraft 1907–1947<ref name=Bowers>{{cite book |last1=Bowers |first1=Peter M. |title=Curtiss aircraft, 1907-1947 |date=1979 |publisher=Putnam |location=London |isbn=0370100298 |pages=439–440}}</ref> |
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|plane or copter?=plane |
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|prime units?=imp |
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|jet or prop?=prop |
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<!-- |
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|ref= |
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General characteristics |
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|crew=one, pilot |
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--> |
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|capacity= |
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|crew=1 |
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|payload main= |
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|length ft=37 |
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|payload alt= |
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|length |
|length in=9 |
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|length |
|length note= |
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|span |
|span ft=46 |
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|span |
|span in=0 |
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|span note= |
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|height main= 12 ft 4 in |
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|height |
|height ft=17 |
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|height in=0 |
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|area main= 375 ft² |
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|height note= |
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|area alt= 35 m² |
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|wing area sqft=375 |
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|wing area note= |
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|aspect ratio=<!-- sailplanes --> |
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|airfoil= |
|airfoil= |
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|empty weight |
|empty weight lb=10531 |
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|empty weight |
|empty weight note= |
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|gross weight lb=14950 |
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|gross weight note= |
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|max takeoff weight lb= |
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|useful load main= |
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|max takeoff weight note= |
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|useful load alt= |
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|fuel capacity= |
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|max takeoff weight main= 14,582 lb |
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|max takeoff weight alt= 6614 kg |
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|more general= |
|more general= |
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<!-- |
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|engine (prop)= Wright XR-3350-16 radial eighteen cylinder twin row air-cooled engine |
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Powerplant |
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|type of prop= |
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--> |
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|number of props=1 |
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|eng1 number=1 |
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|power main= 2,300 hp |
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|eng1 name=[[Wright XR-3350-16]] |
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|power alt= 1.7 MW |
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|eng1 type=eighteen cylinder twin row air-cooled [[radial engine]] |
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|power original= |
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|eng1 hp= |
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|max speed main= 317 mph at sea level, 424 mph at 32,000 ft |
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|max speed alt= 510 km/h at sea level, 682 km/h at 9,800 m |
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|cruise speed main= |
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|cruise speed alt= |
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|stall speed main= |
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|stall speed alt= |
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|never exceed speed main= |
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|never exceed speed alt= |
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|range main= 1,355 statute miles at 162 mph |
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|range alt= 2181 km at 260 km/h |
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|ceiling main= 39,500 ft |
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|ceiling alt= 12,000 m |
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|climb rate main= 2,700 ft/min |
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|climb rate alt= 820 m/min |
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|loading main= |
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|loading alt= |
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|thrust/weight= |
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|power/mass main= |
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|power/mass alt= |
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|more performance= |
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|armament= |
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* 4 × wing mounted 20 mm cannon (planned) |
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|avionics= |
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}} |
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{{aero-specs}} |
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|prop blade number=6 |
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==References== |
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|prop name=contra-rotating constant-speed propeller |
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====Notes==== |
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|prop dia ft=<!-- propeller aircraft --> |
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{{Reflist}} |
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|prop dia in=<!-- propeller aircraft --> |
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====Bibliography==== |
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|prop dia note= |
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{{refbegin}} |
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<!-- |
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* Bowers, Peter M. ''Curtiss Aircraft, 1907-1947''. London, UK: Putnam & Company Ltd., 1979. ISBN 0-370-10029-8. |
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Performance |
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* Green, William. ''War Planes of the Second World War - Fighters, vol. 4''. London, UK: MacDonald, 1961. ISBN 0-356-01448-7. |
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--> |
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* Green, William and Swanborough, Gordon. ''WW2 Aircraft Fact Files: US Navy and marine Corps Fighters''. London, UK: Macdonald and Jane's Publishers Ltd., 1976. ISBN 0-356-08222-9. |
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|max speed mph=418 |
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{{refend}} |
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|max speed note=at {{cvt|32000|ft}} |
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|cruise speed mph=172 |
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|cruise speed note= |
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|stall speed mph= |
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|stall speed note= |
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|never exceed speed mph= |
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|never exceed speed note= |
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|range miles=1530 |
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|range note= |
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|combat range miles= |
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|combat range note= |
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|ferry range miles= |
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|ferry range note= |
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|endurance=<!-- if range unknown --> |
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|ceiling ft=39800 |
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|ceiling note= |
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|g limits=<!-- aerobatic --> |
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|roll rate=<!-- aerobatic --> |
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|climb rate ftmin=2700 |
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|climb rate note= |
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|time to altitude= |
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|wing loading lb/sqft= |
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|wing loading note= |
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|fuel consumption lb/mi= |
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|power/mass= |
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|more performance= |
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==Related content== |
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<!-- |
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{{aircontent |
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Armament |
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--> |
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|guns= 4 × wing mounted {{cvt|20|mm|3}} cannon (planned) |
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|sequence= |
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}} |
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* [[F11C Goshawk|F11C]] - [[Curtiss F12C|F12C]] - [[Curtiss F13C|F13C]] - '''XF14C''' - [[Curtiss F15C|F15C]] |
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==See also== |
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{{Aircontent |
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|related= |
|related= |
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|similar aircraft= |
|similar aircraft= |
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* [[Boeing F8B]] |
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* [[Hawker Sea Fury]] |
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* [[Focke-Wulf Ta 152|Focke-Wulf Ta 152H]] |
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* [[Nakajima Ki-87]] |
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|lists= |
|lists= |
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* [[List of fighter aircraft]] |
* [[List of fighter aircraft]] |
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* [[List of |
* [[List of United States Navy aircraft designations (pre-1962)]] |
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|see also= |
|see also= |
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}} |
}} |
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==References== |
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{{USN fighters}} |
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{{commons category|Curtiss XF14C}} |
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===Notes=== |
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[[Category:United States fighter aircraft 1930-1939|FC14, Curtiss]] |
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{{Reflist}} |
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===Bibliography=== |
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{{Refbegin}} |
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* Bowers, Peter M. ''Curtiss Aircraft, 1907–1947''. London, UK: Putnam & Company Ltd., 1979. {{ISBN|0-370-10029-8}}. |
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* Green, William. ''War Planes of the Second World War - Fighters, vol. 4''. London, UK: MacDonald, 1961. {{ISBN|0-356-01448-7}}. |
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* Green, William and Swanborough, Gordon. ''WW2 Aircraft Fact Files: US Navy and marine Corps Fighters''. London, UK: Macdonald and Jane's Publishers Ltd., 1976. {{ISBN|0-356-08222-9}}. |
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{{Refend}} |
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{{Curtiss aircraft}} |
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{{USN fighters}} |
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[[Category:1940s United States fighter aircraft|Curtiss FC14]] |
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[[ja:F14C (戦闘機)]] |
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[[Category:Low-wing aircraft]] |
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[[Category:Single-engined tractor aircraft]] |
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[[Category:Curtiss aircraft|F14C]] |
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[[Category:Aircraft with contra-rotating propellers]] |
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[[Category:Aircraft first flown in 1944]] |
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Latest revision as of 20:31, 31 July 2022
| XF14C | |
|---|---|
| |
| Role | Carrier-based fighter |
| National origin | United States |
| Manufacturer | Curtiss-Wright |
| First flight | July 1944 |
| Status | Canceled |
| Primary user | US Navy |
| Number built | 1 |
The Curtiss XF14C was an American naval fighter aircraft. It was developed by Curtiss-Wright in response to a request by the United States Navy in 1941 to produce a new shipboard high-performance fighter aircraft.
Design and development[edit]
In 1941 the US Navy requested a better-performing carrier-based fighter plane, to be powered by the proposed high performance 24-cylinder liquid cooled Lycoming XH-2470 Hyper engine. This was an unusual step for the Navy, which had been adamant to that time that all its aircraft use air-cooled radial engines.
On June 30, 1941 a contract for two prototype aircraft, designated the XF14C-1, was awarded to the Curtiss-Wright company. On the same date prototype development contracts were also awarded to Grumman Aircraft Engineering Corporation for the single-engine XF6F-1 and the twin engine XF7F-1, both of which would use air-cooled Pratt & Whitney R-2800 Double Wasp radial engines.
Early in the development the Navy requested better altitude performance and, in view of unsatisfactory progress in the development of the XH-2470 engine, Curtiss adapted the design of the aircraft around the new turbocharged Wright R-3350 Duplex-Cyclone air-cooled radial engine. The aircraft equipped with this eighteen-cylinder twin-row radial air-cooled engine and three bladed contra-rotating propellers was designated the XF14C-2. The XF14C-1 was canceled. Also, looking at the problems of operation at altitudes of about 40,000 feet (12,000 m), the Navy also initiated work on a third version with a pressurized cockpit designated the XF14C-3.
Ultimately, only the XF14C-2 prototype was completed, flying for the first time in July 1944. Moreover, disappointment with performance estimates and delays with the availability of the XR-3350-16 engine coupled with the evaporating tactical need for an extremely high-altitude fighter led to cancellation of the development.
Specifications (XF14C-2)[edit]
Data from Curtiss Aircraft 1907–1947[1]
General characteristics
- Crew: 1
- Length: 37 ft 9 in (11.51 m)
- Wingspan: 46 ft 0 in (14.02 m)
- Height: 17 ft 0 in (5.18 m)
- Wing area: 375 sq ft (34.8 m2)
- Empty weight: 10,531 lb (4,777 kg)
- Gross weight: 14,950 lb (6,781 kg)
- Powerplant: 1 × Wright XR-3350-16 eighteen cylinder twin row air-cooled radial engine
- Propellers: 6-bladed contra-rotating constant-speed propeller
Performance
- Maximum speed: 418 mph (673 km/h, 363 kn) at 32,000 ft (9,800 m)
- Cruise speed: 172 mph (277 km/h, 149 kn)
- Range: 1,530 mi (2,460 km, 1,330 nmi)
- Service ceiling: 39,800 ft (12,100 m)
- Rate of climb: 2,700 ft/min (14 m/s)
Armament
- Guns: 4 × wing mounted 20 mm (0.787 in) cannon (planned)
See also[edit]
Aircraft of comparable role, configuration, and era
Related lists
References[edit]
Wikimedia Commons has media related to Curtiss XF14C.
Notes[edit]
- ^ Bowers, Peter M. (1979). Curtiss aircraft, 1907-1947. London: Putnam. pp. 439–440. ISBN 0370100298.
Bibliography[edit]
- Bowers, Peter M. Curtiss Aircraft, 1907–1947. London, UK: Putnam & Company Ltd., 1979. ISBN 0-370-10029-8.
- Green, William. War Planes of the Second World War - Fighters, vol. 4. London, UK: MacDonald, 1961. ISBN 0-356-01448-7.
- Green, William and Swanborough, Gordon. WW2 Aircraft Fact Files: US Navy and marine Corps Fighters. London, UK: Macdonald and Jane's Publishers Ltd., 1976. ISBN 0-356-08222-9.