Armstrong Siddeley Genet

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The Armstrong Siddeley Genet was a five-cylinder, air-cooled, radial engine for aircraft use built in the UK, first run in 1928. It developed 88 hp at 2,200 rpm and was a popular light airplane type.

[edit] Specifications

• Bore: 101.6 mm (4 in)
• Stroke: 101.6 mm (4 in)
• Displacement:4.3 Liters (251.4 in)
• Weight: 92kg (203 lbs)
• Power: (88 hp) at 2,200 rpm
• Compression 5.25:1

[edit] Applications

• Avro Avian
• ANEC IV
• Blackburn Bluebird
• Cierva autogyros. C.9, C.10 and C.19
• De Havilland Moth
• Junkers A50 Junior
• Klemm kl25
• Parnall Imp
• Robinson Redwing
• Miles Martlett
• Westland Widgeon
• Westland-Hill Pterodactyl

[edit] References

• Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens, 18. 

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