Agusta GA.70: Difference between revisions
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==References== |
==References== |
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* Erickson, Jack. ''[http://home. |
* Erickson, Jack. ''[http://home.comcast.net/~aeroengine/ Horizontally-Opposed Piston Aero Engines]'' |
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Revision as of 22:55, 13 August 2007
The Agusta GA.70 was a 4-cylinder, air-cooled, horizontally-opposed engine developed in Italy for light aircraft and helicopter use. It was produced in the 1950s and 60s.
Applications
General characteristics
- Type: 4-cylinder air-cooled horizontally opposed aircraft piston engine
- Bore: 92 mm (3.6 in)
- Stroke: 86.5 mm (3.4 in)
- Displacement: 2.3 L (140 in³)
- Dry weight: 176 lb (80 kg)
Components
- Cooling system: Air-cooled
Performance
- Power output: 54 kW (72 hp) at 3,100 rpm
References
- Erickson, Jack. Horizontally-Opposed Piston Aero Engines