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