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RAF 3

From PlaneSpottingWorld, for aviation fans everywhere

The RAF 3 was a British liquid-cooled, V-12 engine developed for aircraft use during World War I. Based on the eight–cylinder RAF 1 it was designed by the Royal Aircraft Factory but produced by the two British companies of Armstrong Whitworth and Napier & Son. The RAF 7 was a high compression version of the same engine.[1]

Variants

RAF 3
1914 - Prototype engine, 200 horsepower (150 kW).
RAF 3a
1914 - Main production variant, increased bore, 260 horsepower (194 kW). 29 built by Armstrong Whitworth, 260 built by Napier & Son.
RAF 7
300 horsepower (224 kW) high compression version with high-lift camshafts.

Applications

Specifications (RAF 3a)

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See also

Related development

Related lists

References

Notes

  1. Gunston, 1989, p. 156.

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.

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