- Cranfield A1
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Cranfield A1 Role Aerobatic monoplane National origin United Kingdom Manufacturer Cranfield Institute of Technology First flight 23 August 1967 Number built 1 The Cranfield A1 is a British single-seater aerobatics monoplane, powered by a single Rolls Royce Continental IO-360. The Cranfield A1 is a low-wing cantilever monoplane with a fixed tailwheel landing gear.
Specifications
Data from [1]
General characteristics
- Crew: 1
- Length: 6.83 m (26.41 ft)
- Wingspan: 10 m (32.80 ft)
- Height: 2.89 m (9 ft 6 in)
- Wing area: 15 m² (161.46 ft²)
- Powerplant: 1 × [, ()
Performance
- Maximum speed: 132 mph (245 km/h)
- Service ceiling: 8.858 m (2,700 ft)
- Rate of climb: 7.30 m/s (1437.01 ft/s)
References
Lists relating to aviation General Aircraft (manufacturers) · Aircraft engines (manufacturers) · Airlines (defunct) · Airports · Civil authorities · Museums · Registration prefixes · Rotorcraft (manufacturers) · TimelineMilitary Accidents/incidents Records Categories:- British sport aircraft 1960–1969
- 1960s aircraft stubs
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