Top Qs
Timeline
Chat
Perspective
Mistral G-230-TS
From Wikipedia, the free encyclopedia
Remove ads
The Mistral G-230-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
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)
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
Related lists
References
External links
Wikiwand - on
Seamless Wikipedia browsing. On steroids.
Remove ads