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Sodemo V2-1.2
French aircraft engine From Wikipedia, the free encyclopedia
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The Sodemo V2-1.2 is a French aircraft engine, designed and produced by Sodemo of Magny-Cours, for use in light aircraft.[1]
Design and development
The engine is a 90° V-twin-cylinder four-stroke, 1,200 cc (73.2 cu in) displacement, liquid-cooled, petrol 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: petrol
- Cooling system: liquid
Performance
- Power output: 136 hp (101 kW)
See also
Related development
Related lists
References
External links
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