Sodemo V2-1.0 Explained
The
Sodemo V2-1.0 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, 9921NaN1 displacement, liquid-cooled, petrol engine design, with a mechanical gearbox reduction drive. It employs dual capacitor discharge ignition and produces 1020NaN0 at 6500 rpm.[1]
Notes and References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 256-257. Flying Pages Europe SARL, 2015.
