Sodemo V2-1.0
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The Sodemo V2-1.0 is a French
aircraft engine An aircraft engine, often referred to as an aero engine, is the power component of an aircraft propulsion system. Most aircraft engines are either piston engines or gas turbines, although a few have been rocket powered and in recent years many ...
, 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 A four-stroke (also four-cycle) engine is an internal combustion (IC) engine in which the piston completes four separate strokes while turning the crankshaft. A stroke refers to the full travel of the piston along the cylinder, in either directio ...
, displacement, liquid-cooled, gasoline 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


External links

*{{Official website, http://www.sodemo.com/en/14/the-v2-engine.html Sodemo aircraft engines Liquid-cooled aircraft piston engines 2010s aircraft piston engines