| V2-1.0 | |
|---|---|
| Type | Aircraft engine |
| National origin | France |
| Manufacturer | Sodemo |
The Sodemo V2-1.0 is a French aircraft engine, designed and produced by Sodemo of Magny-Cours, for use in light aircraft. [1]
The engine is a 90° V-twin-cylinder four-stroke, 992 cc (60.5 cu in) displacement, liquid-cooled, petrol engine design, with a mechanical gearbox reduction drive. It employs dual capacitor discharge ignition and produces 102 hp (76 kW) at 6500 rpm. [1]
Data from Tacke [1]
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