The Mistral G-300 is a Swiss aircraft engine designed and produced by Mistral Engines of Geneva for use in light aircraft.
[1] The engine is a three-rotor, 3X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline Wankel engine design, with a mechanical gearbox reduction drive.
It employs dual electronic ignition systems and produces 300 hp (224 kW) at 2250 rpm.
[1] Data from Tacke[1] Related lists