Harman Patil (Editor)

Curtiss XF14C

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Top speed
  
673 km/h

Length
  
12 m

Manufacturer
  
Curtiss-Wright

Wingspan
  
14 m

First flight
  
July 1944

Curtiss XF14C Curtiss XF14C CarrierBorne Fighter Prototype Image

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.

Contents

Curtiss XF14C CurtissWright XF14C2 The Curtiss XF14C was an American n Flickr

Design and development

Curtiss XF14C Curtiss XF14C2 Catalog 00019848 Manufacturer Curtis Flickr

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.

Curtiss XF14C httpsuploadwikimediaorgwikipediacommonsthu

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.

Curtiss XF14C Flightdeck Friday Curtiss XF14C2 Steeljaw Scribe

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.

Curtiss XF14C Curtiss XF14C Info

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)

Data from Curtiss Aircraft 1907–1947

General characteristics

  • Crew: one
  • Length: 37 ft 9 in (11.5 m)
  • Wingspan: 46 ft (14.02 m)
  • Height: 17 ft (5.18 m)
  • Wing area: 375 ft² (34.83 m²)
  • Empty weight: 10,531 lb (4,777 kg)
  • Max. takeoff weight: 14,950 lb (6,781 kg)
  • Powerplant: 1 × Wright XR-3350-16 eighteen cylinder twin row air-cooled radial engine, 2,300 hp (1,716 kW)
  • Performance

  • Maximum speed: 418 mph (363 knots, 673 km/h) at 32,000 ft (9,800 m)
  • Cruise speed: 172 mph (150 knots, 277 km/h)
  • Range: 1,530 mi (1,330 nmi, 2,462 km)
  • Service ceiling: 39,800 ft (12,100 m)
  • Rate of climb: 2,700 ft/min (13.7 m/s)
  • Armament

  • Guns: 4 × wing mounted 20 mm cannon (planned)
  • References

    Curtiss XF14C Wikipedia