SPA 6A
| 6A | |
|---|---|
.JPG) | |
| S.P.A. 6A engine on display at the Gianni Caproni Museum of Aeronautics | |
| Type | Water-cooled Piston aero engine |
| National origin | Italy |
| Manufacturer | Società Piemontese Automobili (S.P.A.) |
| First run | c.1916 |
The S.P.A. 6A was an Italian aero engine of the World War I era. It was a water-cooled inline six-cylinder engine that produced 220 horsepower (164 kW).
Applications
- Ansaldo A.1 Balilla
- Ansaldo SVA
- Bartel BM.5
- Breda A.2
- Breda A.3
- Breda A.9 and A.9bis
- CANT 7ter
- Caproni Ca.61a
- Caproni Ca.66
- SIAI S.50
Specifications
Data from Jane's.[1]
General characteristics
- Type: Inline six-cylinder piston engine
- Bore: 135 mm (5.31 in)
- Stroke: 170 mm (6.69 in)
Components
- Valvetrain: SOHC, two valves per cylinder
- Fuel system: Twin Zenith carburettors
- Cooling system: Water-cooled
- Reduction gear: Direct-drive
- Twin Marelli ignition magnetos
Performance
- Power output: 164 kW (220 hp) at 1,600 rpm
See also
- Comparable engines
- Related lists
References
 |
Wikimedia Commons has media related to SPA 6A. |
- Notes
- ↑ Jane's 1993, p. 316.
- Bibliography
- Jane's Fighting Aircraft of World War I. London. Studio Editions Ltd, 1993. ISBN 1-85170-347-0
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