Mistral G-300

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G-300
Type Aircraft engine
National origin Switzerland
Manufacturer Mistral Engines

The Mistral G-300 is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.[1]

Design and development[edit]

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. It employs dual electronic ignition systems and produces 300 hp (224 kW) at 2250 rpm.[1]

Applications[edit]

Specifications (G-300)[edit]

Data from Tacke[1]

General characteristics

  • Type: Three rotor Wankel aircraft engine
  • Displacement: 3X3X654 cc (39.9 cu in)
  • Dry weight: 177 kg (390.2 lb)

Components

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

Performance

  • Power output: 300 hp (224 kW)

See also[edit]

Related lists

References[edit]

  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[edit]