Mistral G-200

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

G-200
Type	Aircraft engine
National origin	Switzerland
Manufacturer	Mistral Engines

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

• Type: Twin rotor Wankel aircraft engine
• Displacement: 2X3X654 cc (39.9 cu in)
• Dry weight: 132 kg (291.0 lb)

Components

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

Performance

• Power output: 150 hp (112 kW)

See also

Related lists

• List of aircraft engines