North American FJ-1 Fury
The North American FJ-1 Fury was the first operational jet aircraft in United States Navy service, and was developed by North American Aviation as the NA-135. The FJ-1 was an early transitional jet of limited success which carried over similar tail surfaces, wing, and canopy derived from the piston-engined P-51D Mustang. The evolution of the design to incorporate swept wings would become the basis for the land-based XP-86 prototype - itself originally designed with a very similar straight-wing planform to the FJ-1 airframe - of the United States Air Force's enormously influential F-86 Sabre, which in turn formed the basis for the Navy's carrier-based North American FJ-2/-3 Fury.
|An FJ-1 Fury of the US Navy|
|National origin||United States|
|Manufacturer||North American Aviation|
|First flight||11 September 1946|
|Primary user||United States Navy|
|Number built||33 (including prototypes)|
|Developed into||North American F-86 Sabre|
Design and developmentEdit
Ordered in late 1944 as the XFJ-1 in competition with proposals from Douglas and Vought, the Fury began as a straight-wing, tricycle gear fighter with a single turbojet passing through the fuselage. The wing, empennage, and canopy strongly resembled that of the piston-engined P-51D Mustang, North American Aviation's highly successful World War II fighter, enclosing a relocated cockpit accommodation further forward in relation to the Mustang's design, to ensure good forward pilot visibility for carrier operations.
The first flight of the prototype XFJ-1 took place on 11 September 1946, with the first of 30 deliveries beginning in October 1947. Flown by Navy squadron VF-5A, the FJ-1 made the USN's first operational aircraft carrier landing with a jet fighter at sea[N 1] on 10 March 1948 aboard USS Boxer, pioneering US jet-powered carrier operations and underscoring the need for catapult-equipped carriers. The Fury was capable of launching without catapult assistance, but on a crowded flight deck the capability was of limited use. Taking off without a catapult launch limited the FJ-1 to a perilous, slow climb that was considered too risky for normal operations.
As German research into swept wing aerodynamics was not yet available when the design was finalized, the FJ-1 used a straight wing. No provision for wing-folding had been made as dive brakes mounted in the wings made that option unfeasible. In order to conserve carrier deck space, a unique "kneeling" nose undercarriage along with a swivelling "jockey wheel" allowed the FJ-1 to be stacked tail-high, close to another FJ-1.
Although ordered into production, the initial order for 100 units was trimmed to only 30 aircraft which were mainly used in testing at NAS North Island, California. VF-5A, soon redesignated as VF-51, operated the type in service beginning in August 1948. Although VF-51 went to sea on Boxer by May 1949, the FJ-1s were phased out in favor of the new F9F-2 Panther.
Ending its service career in U.S. Naval Reserve units, the FJ-1 eventually was retired in 1953. The one highlight in its short service life was VF-51's win in the Bendix Trophy Race for jets in September 1948. The unit entered seven FJ-1s, flying from Long Beach, California to Cleveland, Ohio, with VF-51 aircraft taking the first four places, ahead of two California Air National Guard Lockheed F-80 Shooting Stars.
- Prototype aircraft, powered by a 3,820 lbf (17 kN) General Electric J35-GE-2 turbojet engine, three built.
- FJ-1 Fury
- Single-seat fighter aircraft, powered by a 4,000 lbf (17.8 kN) Allison J35-A-2 turbojet engine, armed with six 0.50 in (12.7 mm) machine guns, 30 built a further 70 were cancelled.
Aircraft on displayEdit
- Crew: 1
- Length: 34 ft 5 in (10.48 m)
- Wingspan: 38 ft 2 in (11.63 m)
- Height: 14 ft 10 in (4.52 m)
- Wing area: 221 ft2 (20.5 m2)
- Empty weight: 8,843 lb (4,010 kg)
- Loaded weight: 15,118 lb (6,854 kg)
- Fuel provisions Internal fuel load: 465 gal (1,743 l), Wing Tip Tanks: 2 × 170 gal (644 l)
- Powerplant: 1 × Allison J35-A-2 turbojet, 4,000 lbf (17.8 kN)
- Maximum speed: 547 mph at 9,000 ft (880 km/h at 2,743 m)
- Range: 1,496 mi, (2,407 km) 1,496 mi (2,407 km) with external tanks
- Service ceiling: 32,000 ft. (9,753 m)
- Rate of climb: 3,300 ft/min at sea level (1,005 m/min)
- Thrust/weight: 0.38
- Stalling speed (power off): 121 mph (106 kn, 194 km/h)
- North American P-51 Mustang
- North American F-86 Sabre
- North American FJ-2/-3 Fury
- North American FJ-4 Fury
Aircraft of comparable role, configuration and era
- de Havilland Sea Vampire
- Gloster E.1/44
- Hawker Sea Hawk
- McDonnell FH Phantom
- Supermarine Attacker
- Vought F6U Pirate
- Saab 29 Tunnan
- "The FJ-1 Fury." Archived 2002-10-16 at the Wayback Machine f-86.tripod.com. Retrieved: 29 April 2008.
- "FJ Fury." Archived 2003-02-07 at the Wayback Machine boeing.com. Retrieved: 29 April 2008.
- "FJ Fury." globalsecurity.org. Retrieved: 29 April 2008.
- Andrade 1979, p. 190
- "FJ Fury/120349". Archived 2015-12-18 at the Wayback Machine Yanks Air Museum. Retrieved: 29 October 2012.
- "FJ-1 Fury/120351". NASM. Retrieved: 17 January 2011.
- Andrade, John M., U.S. Military Aircraft Designations and Serials since 1909. Leicester, England: Midland Counties Publishing, 1979 ISBN 0-904597-22-9
- Taylor, John, W.R., ed. Jane's All the World's Aircraft 1965-1966. London: Jane's All the World's Aircraft, 1967. ISBN 0-7106-1377-6.
- Wagner, Ray. The North American Sabre. London: Macdonald, 1963. No ISBN.
- Winchester, Jim, ed. Military Aircraft of the Cold War (The Aviation Factfile). London: Grange Books plc, 2006. ISBN 1-84013-929-3.
Media related to North American FJ-1 Fury at Wikimedia Commons