Mistral G-200

The Mistral G-200 is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.

Design and development
The engine is a twin-rotor, 2X3X654 cc 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 150 hp.