Mistral G-360-TS
| G-360-TS | |
|---|---|
| Type | Aircraft engine |
| National origin | Switzerland |
| Manufacturer | Mistral Engines |
The Mistral G-360-TS is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.[1]
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 three-rotor, 3X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline Wankel engine design, with a mechanical gearbox reduction drive with a reduction ratio of 2.82:1. It employs dual electronic ignition systems and produces 360 hp (268 kW) at 2250 rpm.[1]
Specifications (G-360-TS)[edit]
Data from Tacke[1]
General characteristics
- Type: Twin rotor Wankel aircraft engine
- Displacement: 3X3X654 cc (39.9 cu in)
- Dry weight: 190 kg (418.9 lb)
Components
- Fuel type: gasoline
- Cooling system: liquid
- Reduction gear: mechanical gearbox
Performance
- Power output: 360 hp (268 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.