Mistral G-200
From Wikipedia, the free encyclopedia
| G-200 | |
|---|---|
| Type | Aircraft engine |
| National origin | Switzerland |
| Manufacturer | Mistral Engines |
The Mistral G-200 is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.[1]
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)