avia.wikisort.org - Aeroplane
The Northrop N-102 Fang was a fighter aircraft design created by Northrop Corporation and proposed to the United States Air Force in 1953.
| N-102 Fang | |
|---|---|
 | |
| Patent images of the N-102 design | |
| Role | Light fighter |
| National origin | United States |
| Manufacturer | Northrop Corporation |
| Status | Project only |
Design and development
In the early 1950s, concerns grew in the United States about the growing weight, complexity and cost of modern fighter aircraft, and in late 1952, Northrop started a design study for a simple, lightweight, supersonic fighter aircraft, the N-102 Fang, with the design team headed by Welko E. Gasich, Northrop's Chief of Advanced Design.[1][2][3] On 12 December that year, the United States Air Force (USAF) issued a requirement for a lightweight air superiority aircraft to replace the F-100 supersonic fighter. The new aircraft was expected to enter service in 1957 and was required to have a speed of at least Mach 1.3 at 35,000 ft (11,000 m) and a combat radius of 400 mi (650 km). Northrop proposed the N-102 to meet the requirement, while other competitors were from Lockheed (the CL-246), North American Aviation (the NA-212) and Republic Aviation (the AP-55).[4]
The N-102 had a shoulder-mounted delta wing and a small all-moving tailplane mounted behind the wing. It would be powered by a single turbojet mounted in the lower aft fuselage which was supplied by air from a variable-geometry ventral air inlet. This promised smoother, more efficient airflow to the engine at the risk of being more vulnerable to ingestion of foreign objects and damage to the engine.[5][6] A number of different engines were proposed, including the Pratt & Whitney J57, the Wright J65 (a license-produced derivative of the British Armstrong Siddeley Sapphire), the Wright J67 (a license-built Bristol Olympus or the General Electric J79, with all of the engines giving an estimated speed of at least Mach 2.[7]
In early 1953, the USAF selected Lockheed's CL-246, which became the Lockheed F-104 Starfighter, but Northrop at first continued work on the N-102 with the hope of gaining export orders, building a mock-up of the aircraft in USAF colors.[8] However, the use of a single, large engine meant that the aircraft could not be as light or cheap as Northrop wanted, and Northrop stopped work on the N-102 during 1954.[5][2][9] Northrop continued work on lightweight fighters, basing its further studies on the use of two small General Electric J85 engines, which allowed a much lighter and cheaper aircraft,[5] with Northrop's design team believing that twin engines would increase the reliability and safety margin.[10] The J85-powered design studies eventually formed the basis of the F-5 fighter family.[11][12][13]
The design was the subject of a 1957 design patent.[14]
Specifications (J79 engine - performance estimated)
Data from Northrop N-102 "Fang"[7]
General characteristics
- Crew: 1
- Length: 42 ft 7 in (12.97 m)
- Wingspan: 30 ft 8 in (9.34 m)
- Wing area: 270.0 sq ft (25.08 m2)
- Gross weight: 18,735 lb (8,498 kg)
- Powerplant: 1 × General Electric J79-GE-1 , 9,300 lbf (41 kN) thrust dry, 14,400 lbf (64 kN) with afterburner
Performance
- Maximum speed: Mach 2
- Combat range: 390 mi (630 km, 340 nmi)
- Ferry range: 2,029 mi (3,266 km, 1,763 nmi)
- Service ceiling: 59,000 ft (18,000 m)
- Rate of climb: 44,500 ft/min (226 m/s)
Armament
- Guns: 1× 20 mm M61 Vulcan 6-barreled rotary cannon or 2× 20mm M39 Revolver cannon
- Missiles: 4× AIM-4 Falcon air-to-air missiles
See also
Related development
Aircraft of comparable role, configuration, and era
References
Media related to N-102 Fang at Wikimedia Commons
- Scutts 1986, pp. 6–7.
- Lake & Hewson 1996, p. 48.
- Pelletier 2012, pp. 71–72.
- Pelletier 2012, p. 72.
- Scutts 1986, p. 7.
- Pelletier 2012, pp. 72–73.
- Pelletier 2012, p. 73.
- Pelletier 2012, pp. 73–74.
- Pelletier 2012, p. 74.
- General Electric Company (1979). Seven decades of progress: a heritage of aircraft turbine technology. Fallbrook, CA: Aero Publishers. p. 108. ISBN 0-8168-8355-6.
- Lake & Hewson 1996, pp. 48–49.
- Scutts 1986, pp. 7–8.
- Lorell, Mark A.; Levaux, Hugh P. (1998). The cutting edge: a half century of fighter aircraft R&D. RAND Corporation. p. 114. ISBN 0-8330-2595-3.
- US design 180297, "Aircraft", published 1957-05-14, assigned to Northrop Aircraft Inc.
- Lake, Jon; Hewson, Richard (Summer 1996). "Northrop F-5". World Air Power Journal. Vol. 25. London: Aerospace Publishing. pp. 46–109. ISBN 1-874023-79-4. ISSN 0959-7050.
- Pelletier, Alain (November 2012). "Northrop N-102 "Fang": Le chasseur petite échelle de Northrop". Le Fana de l'Aviation (in French). No. 516. pp. 70–75.
- Scutts, Jerry (1986). Northrop F-5/F-20. London: Ian Allan. ISBN 0-7110-1576-7.
На других языках
- [en] Northrop N-102 Fang
[fr] Northrop N-102 Fang
Le Northrop N-102 Fang est un prototype d'avion de chasse développé par Northrop Corporation et proposé à l'United States Air Force en 1953[1].Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
WikiSort.org - проект по пересортировке и дополнению контента Википедии