Mistral G-200 Explained
The
Mistral G-200 is a
Swiss aircraft engine, designed and produced by
Mistral Engines of
Geneva for use in
light aircraft.
[1] Design and development
The engine is a twin-rotor, 2X3X6541NaN1 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 1500NaN0.[1]
Notes and References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015.
