Agusta GA.140
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| GA.140 | |
|---|---|
| Type | 4-cyl. horizontally opposed air-cooled piston engine |
| National origin | Italy |
| Manufacturer | Agusta |
The Agusta GA.140/V is a 4-cylinder, air-cooled, horizontally opposed engine mounted vertically, developed in Italy for helicopter use and produced from 1962 to 1969.
Specifications (G.A.140/V)
Data from Jane's All the World's Aircraft 1962–63[1]
General characteristics
- Type: 4-cylinder air-cooled horizontally opposed helicopter piston engine
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- Stroke: Script error: No such module "convert".
- Displacement: Script error: No such module "convert".
- Length: Script error: No such module "convert".
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- Dry weight: Script error: No such module "convert". dry
- Designer: M. Ginnini
Components
- Valvetrain: pushrod operated overhead valve, 2x inlet + 2x exhaust per cylinder
- Fuel system: Marvel-Schebler MA 4.5 carburettor
- Fuel type: 91 octane minimum
- Oil system: Pressure lubrication with a gear driven pump
- Cooling system: Air-cooled
Performance
- Power output: Script error: No such module "convert". at 3,200 rpm
- Specific power: 28.173 kW/L (0.619 hp/cu in)
- Compression ratio: 8.2:1
- Power-to-weight ratio: 0.887 kW/kg (0.5395 hp/lb)
Applications
Notes
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References
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- Erickson, Jack. Horizontally-Opposed Piston Aero Engines
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