G-200 | |
---|---|
Type | Aircraft engine |
National origin | Switzerland |
Manufacturer | Mistral Engines |
The Mistral G-200 is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft. [1]
The engine is a twin-rotor, 2X3X654 cc (39.9 cu in) 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 (112 kW). [1]
Data from Tacke [1]
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