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By March 2018 the engine was no longer advertised on the company website and seems to be out of production.
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The engine is a three-rotor, 3X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline
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systems and produces 360 hp (268 kW) at 2250 rpm.
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Swiss aircraft engine made by
Mistral Engines of Geneva
104:with a reduction ratio of 2.82:1. It employs dual
233:, pages 260-261. Flying Pages Europe SARL, 2015.
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231:World Directory of Light Aviation 2015-16
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140:3X3X654 cc (39.9 cu in)
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229:Tacke, Willi; Marino Boric; et al:
100:design, with a mechanical gearbox
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131:Twin rotor Wankel aircraft engine
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149:190 kg (418.9 lb)
73:, designed and produced by
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190:360 hp (268 kW)
112:Specifications (G-360-TS)
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378:Pistonless rotary engine
373:Mistral aircraft engines
206:List of aircraft engines
259:www.mistral-engines.com
123:General characteristics
92:Design and development
106:electronic ignition
177:mechanical gearbox
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166:Cooling system:
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102:reduction drive
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75:Mistral Engines
71:aircraft engine
55:Mistral Engines
40:National origin
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262:. Retrieved
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136:Displacement
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326:aeroengines
182:Performance
81:for use in
45:Switzerland
367:Categories
212:References
160:Fuel type:
154:Components
145:Dry weight
239:1368-485X
117:Data from
24:G-360-TS
352:G-360-TS
342:G-230-TS
264:28 March
195:See also
162:gasoline
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168:liquid
79:Geneva
347:G-300
337:G-200
129:Type:
119:Tacke
68:Swiss
66:is a
29:Type
266:2018
235:ISSN
62:The
77:of
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220:^
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315:e
308:t
301:v
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