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Mistral G-230-TS

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The Mistral G-230-TS is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.[1]

Quick facts G-230-TS, Type ...

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 twin-rotor, 2X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline Wankel engine design, with a mechanical gearbox reduction drive with a reduction ratio of 2.8:1. It employs dual electronic ignition systems and produces 230 hp (172 kW) at 2515 rpm.[1]

Specifications (G-230-TS)

Data from Tacke[1]

General characteristics

  • Type: Twin rotor Wankel aircraft engine
  • Displacement: 2X3X654 cc (39.9 cu in)
  • Dry weight: 149 kg (328.5 lb)

Components

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

Performance

  • Power output: 230 hp (172 kW)

See also

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