The Sodemo V2-1.0 is a French aircraft engine, designed and produced by Sodemo of Magny-Cours, for use in light aircraft.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 256-257. Flying Pages Europe SARL, 2015.
Design and development The engine is a 90° V-twin-cylinder four-stroke, displacement, liquid-cooled, petrol engine design, with a mechanical gearbox reduction drive. It employs dual capacitor discharge ignition and produces at 6500 rpm.
Specifications (V2-1.0)
See also
References
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