Blackburn Cirrus Bombardier
| Cirrus Bombardier |
|---|
 |
| Type |
Air-cooled 4-cylinder inline piston engine |
| National origin |
United Kingdom |
| Manufacturer |
Blackburn Aircraft |
| First run |
c.1954 |
|
|
The Blackburn Cirrus Bombardier was a British, inline, four-cylinder aircraft engine that was developed and built by the Blackburn Aircraft company in the mid-1950s. The engine featured fuel injection.
Variants
- Cirrus Bombardier 203
- Military version, 203 hp (151 kW).
- Cirrus Bombardier 702
- Civil version, 180 hp (134 kW).
Applications
Specifications (Cirrus Bombardier 203)
Data from Lumsden.[1]
General characteristics
- Type: Inline, air-cooled, inverted 4-cylinder
- Bore: 4.8 in (122 mm)
- Stroke: 5.5 in (140 mm)
- Displacement: 398 cu in (6.5 L)
- Length: 45.3 in (1,151 mm)
- Width: 19 in (483 mm)
- Height: 30.95 in (786 mm)
- Dry weight: 325 lb (147.4 kg)
Components
Performance
See also
- Related development
- Comparable engines
- Related lists
References
Notes
Bibliography
- Oldengine.org
- Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 40.
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
External links
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