Agusta GA.70
From Wikipedia, the free encyclopedia
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.
[edit] Applications
- Agusta A.103
- de Bernardi Aeroscooter
- Phoenix Minor
- Phoenix Major
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
- Specific power:
- Power-to-weight ratio:
[edit] References
- Erickson, Jack. Horizontally-Opposed Piston Aero Engines
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