Bristol Lucifer
From Wikipedia, the free encyclopedia
The Bristol Lucifer was a British three-cylinder, air-cooled, radial engine for aircraft. Built in the UK in the 1920s by the Bristol Aeroplane Company, it produced 100 horsepower (75 kW).
The Lucifer was originally a Cosmos Engineering engine, Cosmos being taken over by Bristol in 1920.
Applications
- Albatros L 69
- Avro 504
- Boulton Paul P.10
- Bristol M.1D
- Bristol Primary Trainer
- Handley Page Hamlet
- LFG V 44
- NVI F.K.29
- Parnall Peto
Specifications (Lucifer 1)
Data from Lumsden[1]
General characteristics
- Type: 3-cylinder air-cooled single-row radial engine
- Bore: 5.75 in (146 mm)
- Stroke: 6.25 in (159 mm)
- Displacement: 487 in³ (8.0 L)
- Diameter: 48 in (1219 mm)
- Dry weight: 324 lb (147 kg)
Components
- Valvetrain: Four valves per cylinder, poppet valve
- Fuel type: Petrol
- Cooling system: Air-cooled
Performance
- Power output: 100 hp (75 kW)
- Compression ratio: 4.8:1
- Power-to-weight ratio: 0.3 hp/lb
See also
- Comparable engines
- Related lists
References
Wikimedia Commons has media related to Bristol Lucifer. |
Notes
- ↑ Lumsden 2003, p. 93.
Bibliography
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
|
|
This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.