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Genet II

Genet II is a piston engine model used in aircraft.

Specifications

Engine Family: piston

Bore: 101.6 millimetre

Compression ratio: 5.2

Cooling system: Air

Cylinder configuration: Radial

Cylinder count: 5

Displacement: 4119 cubic-centimetre

Dry weight: 95 kilogram

Fuel grade: 73/77

Fuel type: Avgas

Max. continuous RPM: 2200

Max. continuous hp: 80 horsepower

Max. takeoff RPM: 2000

Max. takeoff hp: 80 horsepower

Stroke: 101.6 millimetre

Manufacturer

Armstrong Siddeley