Mistral G-200

Last updated

G-200
Type Aircraft engine
National origin Switzerland
Manufacturer Mistral Engines
Unit cost US$31,500 (2015)

The Mistral G-200 is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft. [1]

Switzerland federal republic in Central Europe

Switzerland, officially the Swiss Confederation, is a country situated in western, central, and southern Europe. It consists of 26 cantons, and the city of Bern is the seat of the federal authorities. The sovereign state is a federal republic bordered by Italy to the south, France to the west, Germany to the north, and Austria and Liechtenstein to the east. Switzerland is a landlocked country geographically divided between the Alps, the Swiss Plateau and the Jura, spanning a total area of 41,285 km2 (15,940 sq mi). While the Alps occupy the greater part of the territory, the Swiss population of approximately 8.5 million people is concentrated mostly on the plateau, where the largest cities are to be found: among them are the two global cities and economic centres Zürich and Geneva.

Aircraft engine Engine designed for use in powered aircraft

An aircraft engine is a component of the propulsion system for an aircraft that generates mechanical power. Aircraft engines are almost always either lightweight piston engines or gas turbines, except for small multicopter UAVs which are almost always electric aircraft.

Mistral Engines SA is a Swiss firm formed in 2001 with the purpose of developing engines for light aircraft and helicopters. Its headquarters is in Geneva, Switzerland. A wholly owned subsidiary company is headquartered in DeLand, Florida.

Contents

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]

Wankel engine internal combustion engine using an eccentric rotary design in place of pistons

The Wankel engine is a type of internal combustion engine using an eccentric rotary design to convert pressure into rotating motion.

Reduction drive Device, containing a different gears.

A reduction drive is a mechanical device to shift rotational speed. A planetary reduction drive is a small scale version using ball bearings in an epicyclic arrangement instead of toothed gears.

Specifications (G-200)

Data from Tacke [1]

General characteristics

Components

  • Fuel type: gasoline
  • Cooling system: liquid
  • Reduction gear: integral mechanical gearbox
Propeller speed reduction unit

A propeller speed reduction unit is a gearbox or a belt and pulley device used to reduce the output revolutions per minute (rpm) from the higher input rpm of the powerplant. This allows the use of small displacement internal combustion automotive engines to turn aircraft propellers within an efficient speed range.

Performance

  • Power output: 150 hp (112 kW)

See also

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References

  1. 1 2 3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015. ISSN   1368-485X