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, 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]
Specifications (G-200)
Data from Tacke[1]
General characteristics
Components
- Fuel type: gasoline
- Cooling system: liquid
- Reduction gear: integral mechanical gearbox
- Power output: 150 hp (112 kW)
See also
Related lists
References
- ^ a b c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015. ISSN 1368-485X
External links
