The Mistral G-200 is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015.
Design and development The engine is a twin-rotor, 2X3X displacement, liquid-cooled, gasoline Wankel engine design, with an integral mechanical gearbox reduction drive with a reduction ratio of 2.82:1. It employs dual electronic ignition systems and produces .
Specifications (G-200)
See also
References
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