XF-87 Blackhawk | |
---|---|
Role | Interceptor |
Manufacturer | Curtiss-Wright |
First flight | 5 March 1948 |
Status | Cancelled 10 October 1948 |
Primary user | U.S. Air Force |
Number built | 2 |
Program cost | $11.3 million USD[1] |
Contents
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Design and development
The aircraft started life as a project for an attack aircraft, designated XA-43. When the United States Army Air Forces issued a requirement for a jet-powered all-weather fighter in 1945, the design was reworked for that request.The XP-87 was a large mid-wing aircraft with four engines paired in underwing pods, with a mid-mounted tailplane and tricycle undercarriage. Two crew members (pilot and radio operator) sat side by side under a single canopy. Armament was to be a nose-mounted, powered turret containing four 20 mm (.79 in) cannon, but this was never fitted to the prototypes.
Operational history
The first flight was on 5 March 1948. Although the top speed was slower than expected, the aircraft was otherwise acceptable, and the newly-formed (in September 1947) United States Air Force placed orders for 57 F-87A fighters and 30 RF-87A reconnaissance planes just over a month later. Since the performance problems were due to lack of power, the four Westinghouse XJ34-WE-7 turbojets of the prototypes were to be replaced by two General Electric J35 jets in production models. One of the two XF-87 prototypes was to be converted to the new powerplants for test purposes.At this point, the USAF decided that the Northrop F-89 Scorpion was a more promising aircraft. The F-87 contract was cancelled on 10 October 1948, and both prototypes were scrapped.
Variants
- XP-97 -
- XF-87 -
Specifications (XF-87)
Data from Curtiss Aircraft 1907–1947[3]
General characteristics- Crew: two - pilot, radio operator
- Length: 62 ft 10 in (19.15 m)
- Wingspan: 60 ft 0 in (18.28 m)
- Height: 20 ft 0 in (6.09 m)
- Wing area: 600 ft² (55.74 m²)
- Empty weight: 25,930 lb (11,786 kg)
- Max takeoff weight: 49,900 lb (22,682 kg)
- Powerplant: 4× Westinghouse XJ34-WE-7 turbojets, 3,000 lbf (13.4 kN) each
- Maximum speed: 600 mph (521 knots, 966 km/h)
- Range: 1,000 mi (870 nmi, 1,610 km)
- Service ceiling: 41,000 ft (12,500 m)
- Climb to 35,000 ft (10,700 m): 13.8 min
- Guns: 4 × 20 mm cannon in nose
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