RAF 2
The RAF 2 was a British air-cooled, nine-cylinder radial engine developed for aircraft use just prior to World War I; it was designed and built by the Royal Aircraft Factory.[1]
Applications
Specifications (RAF 2)
Data from Lumsden[2]
General characteristics
- Type: 9-cylinder, single-row, radial engine
- Bore: 3.94 in (100 mm)
- Stroke: 5.51 in (140 mm)
- Displacement: 604.6 cu in (9.9 L)
Components
Performance
See also
- Related lists
References
Notes
- ^ Gunston, 1989, p. 156.
- ^ Lumsden 2003, p. 223.
Bibliography
- Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
|
|
General |
|
|
Military |
|
|
Accidents/incidents |
|
|
Records |
|
|