Logo

Leopard III

Leopard III is a piston engine model used in aircraft.

Specifications

Engine Family: piston

Bore: 152.4 millimetre

Compression ratio: 5.1

Cooling system: Air

Cylinder configuration: Radial

Cylinder count: 14

Displacement: 48650 cubic-centimetre

Dry weight: 772 kilogram

Fuel type: Avgas

Max. continuous RPM: 1700

Max. continuous hp: 800 horsepower

Max. takeoff RPM: 1700

Max. takeoff hp: 800 horsepower

Stroke: 190.5 millimetre

Manufacturer

Armstrong Siddeley