Mistral G-360-TS

The Mistral G-360-TS is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.[1]

G-360-TS
Type Aircraft engine
National origin Switzerland
Manufacturer Mistral Engines

By March 2018 the engine was no longer advertised on the company website and seems to be out of production.[2]

Design and development

The engine is a three-rotor, 3X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline Wankel engine design, with a mechanical gearbox reduction drive with a reduction ratio of 2.82:1. It employs dual electronic ignition systems and produces 360 hp (268 kW) at 2250 rpm.[1]

Specifications (G-360-TS)

Data from Tacke[1]

General characteristics
  • Type: Twin rotor Wankel aircraft engine
  • Displacement: 3X3X654 cc (39.9 cu in)
  • Dry weight: 190 kg (418.9 lb)

Components
  • Fuel type: gasoline
  • Cooling system: liquid
  • Reduction gear: mechanical gearbox

Performance
  • Power output: 360 hp (268 kW)

See also

Related lists

References
  1. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. Mistral Engines. "Our Products". www.mistral-engines.com. Retrieved 28 March 2018.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.