| G-230-TS | |
|---|---|
| Type | Aircraft engine |
| National origin | Switzerland |
| Manufacturer | Mistral Engines |
The Mistral G-230-TS is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.
By March 2018 the engine was no longer advertised on the company website and seems to be out of production.
Design and development
The engine is a twin-rotor, 2X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline Wankel engine design, with a mechanical gearbox reduction drive with a reduction ratio of 2.8:1. It employs dual electronic ignition systems and produces 230 hp (172 kW) at 2515 rpm.
Specifications (G-230-TS)
Data from Tacke
General characteristics
- Type: Twin rotor Wankel aircraft engine
- Displacement: 2X3X654 cc (39.9 cu in)
- Dry weight: 149 kg (328.5 lb)
Components
- Fuel type: gasoline
- Cooling system: liquid
- Reduction gear: mechanical gearbox
Performance
- Power output: 230 hp (172 kW)
See also
Related lists
References
- ^ Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Mistral Engines. "Our Products". www.mistral-engines.com. Retrieved 28 March 2018.
External links
| Mistral Engines aeroengines | |
|---|---|