Armstrong Siddeley Lynx
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The Armstrong-Siddeley Lynx was an aero engine developed by Armstrong Siddeley.
General characteristics
- Type: 7-cylinder radial piston engine
- Bore: 5.5 in
- Stroke: 5.0 in
- Displacement: 12.4 l
- Dry weight: 524.79 lbs
Components
- Cooling system: air-cooled
Performance
- Power output: 187 hp @ 1,700 rpm(cruise) 215hp@1,900 rpm (max)
- Specific power:
- Compression ratio: 5.0:1
- Power-to-weight ratio:
[edit] Use
[edit] See also
[edit] References
Virtual Aviation Museum (www.luftfahrtmuseum.com)
Armstrong Siddeley aero-engines
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