The Mistral G-230-TS is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.[1]
| G-230-TS | |
|---|---|
| Type | Aircraft engine |
| National origin | Switzerland |
| Manufacturer | Mistral Engines |
By March 2018 the engine was no longer advertised on the company website and seems to be out of production.[2]
Design and development edit
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.[1]
Specifications (G-230-TS) edit
Data from Tacke[1]
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 edit
Related lists
References edit
- ^ a b c 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.