Armstrong Siddeley Leopard
From Wikipedia, the free encyclopedia
The Armstrong Siddeley Leopard was an aero engine developed by Armstrong Siddeley.
[edit] Specifications (Armstrong Siddeley Leopard)
General characteristics
- Type: 14 cylinder twin-row air cooled radial engine
- Bore: 152mm (6 in)
- Stroke: 190mm (7.5 in)
- Displacement: 31.3 Liters (1,909 cu in)
- Dry weight: 665kg (1,466 lb)
Components
- Cooling system: air
Performance
- Power output: 700hp @ 1,650 RPM
- Compression ratio: 5.00
- Specific fuel consumption: 45 gal/hr ( 169 l/std) @ cruise speed
[edit] See also
|
|||||
|
||||||||||||||
