Mistral G-200
# 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.

## 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).

## Specifications (G-200)

Data from Tacke

### 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)
