Sodemo V2-1.2
The Sodemo V2-1.2 is a French aircraft engine, designed and produced by Sodemo of Magny-Cours, for use in light aircraft.[1]
| V2-1.2 | |
|---|---|
| Type | Aircraft engine |
| National origin | France |
| Manufacturer | Sodemo |
Design and development
The engine is a 90° V-twin-cylinder four-stroke, 1,200 cc (73.2 cu in) displacement, liquid-cooled, gasoline engine design, with a mechanical helical-gear gearbox reduction drive. It employs dual capacitor discharge ignition and produces 136 hp (101 kW).[1]
Specifications (V2-1.2)
Data from Tacke[1]
General characteristics
- Type: Twin cylinder, four stroke aircraft engine
- Displacement: 992 cc (60.5 cu in)
Components
- Fuel type: gasoline
- Cooling system: liquid
Performance
- Power output: 136 hp (101 kW)
References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 256-257. Flying Pages Europe SARL, 2015. ISSN 1368-485X
External links
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