The Mistral G-300 is a Swiss aircraft engine designed and produced by Mistral Engines of Geneva for use in light aircraft.[1]
| G-300 | |
|---|---|
| Type | Aircraft engine |
| National origin | Switzerland |
| Manufacturer | Mistral Engines |
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
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