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Mistral G-200

From Wikipedia, the free encyclopedia

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]

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

Performance

  • Power output: 150 hp (112 kW)

See also

Related lists

References

  1. ^ 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

This page was last edited on 29 March 2018, at 11:01
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