Armstrong Siddeley Genet Major

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The Armstrong Siddeley Genet Major was a seven-cylinder, air-cooled, radial engine for aircraft use built in the UK, first run in 1928. It developed 140 hp (104 kW)

[edit] Specifications

• Bore: 135 mm (5.3 in)
• Stroke: 170 mm (6.7 in)
• Displacement: 17.1 L (1,043 cu in)
• Weight: 126 kg (278 lb)
• Power: 82 kW (110 hp) at 1,750 rpm

[edit] Applications

• ANBO V
• Avro 638
• Avro Cadet
• Avro Rota
• Cierva C.30A Autogiro
• Westland IV

[edit] References

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

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