Agusta GA.70
| Agusta GA.70 | |
|---|---|
| Type | 4-cylinder, air-cooled, horizontally opposed engine |
| National origin | Italy |
| Manufacturer | Agusta |
| Designer | M. Ginnini |
| First run | 1955 |
The Agusta GA.70 was a 4-cylinder, air-cooled, horizontally opposed engine developed in Italy for light aircraft and helicopter use. The GA.70/V featured a bottom sump for vertical applications and was rated at 158hp. It was produced in the 1950s and 60s.[1]
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
Applications
References
- ^ Flight. July 1957.
{{cite journal}}: Missing or empty|title=(help)
- Erickson, Jack. Horizontally-Opposed Piston Aero Engines