Mistral G-300
# Mistral G-300

The Mistral G-300 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 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.

## Applications

* Seaflight Shearwater

## Specifications (G-300)

Data from Tacke

### 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)
