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