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| The '''] XF-92''' was the first ] ] aircraft. The design was developed by Dr ] of ] before and during ]. Working with captured data, the ] developed the idea further. | The '''] XF-92''' was the first ] ] aircraft. The design was developed by Dr ] of ] before and during ]. Working with captured data, the ] developed the idea further. | ||
| ] | |||
| Research from the '''XF-92A''' test program was used in the development of Convair's two later delta-winged ]s, the ] and the ], as well as the ] bomber. | Research from the '''XF-92A''' test program was used in the development of Convair's two later delta-winged ]s, the ] and the ], as well as the ] bomber. | ||
Revision as of 00:22, 5 October 2004
The Convair XF-92 was the first American delta-wing aircraft. The design was developed by Dr Alexander Lippisch of Germany before and during World War II. Working with captured data, the U. S. Air Force developed the idea further.
Research from the XF-92A test program was used in the development of Convair's two later delta-winged interceptors, the F-102 Delta Dagger and the F-106 Delta Dart, as well as the B-58 Hustler bomber.
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Specifications (XF-92A)
General Characteristics
- Crew: one pilot
- Length: 42 ft 6 in (12.99 m)
- Wingspan: 31 ft 4 in (9.55 m)
- Height: 17 ft 9 in (5.37 m)
- Wing area: 425 ft² (39.5 m²)
- Empty: 9,078 lb (4,126 kg)
- Loaded: 14,608 lb (6,640 kg)
- Maximum takeoff: lb ( kg)
- Powerplant: 1x Allison J33-A-29 turbojet, 7,500 lb (33.4 kW) thrust
Performance
- Maximum speed: 718 mph (1,149 km/h)
- Range: miles ( km)
- Service ceiling: 50,750 ft (15,472 m)
- Rate of climb: 8,135 ft/min (2,480 m/min)
- Wing loading: 34 lb/ft² (168 kg/m²)
- Thrust-to-Weight: 1:1.1
Armament
Never installed
External links
Related content
Related development:
Comparable aircraft:
Designation sequence: F-89 - XF-90 - XF-91 - XF-92 - YF-93 - F-94 - YF-95
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