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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 twin-rotor, 2X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline
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systems and produces 230 hp (172 kW) at 2515 rpm.
230:, pages 260-261. Flying Pages Europe SARL, 2015.
101:with a reduction ratio of 2.8:1. It employs dual
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228:World Directory of Light Aviation 2015-16
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137:2X3X654 cc (39.9 cu in)
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226:Tacke, Willi; Marino Boric; et al:
97:design, with a mechanical gearbox
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128:Twin rotor Wankel aircraft engine
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146:149 kg (328.5 lb)
70:, designed and produced by
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187:230 hp (172 kW)
109:Specifications (G-230-TS)
20:
375:Pistonless rotary engine
370:Mistral aircraft engines
203:List of aircraft engines
256:www.mistral-engines.com
120:General characteristics
89:Design and development
103:electronic ignition
174:mechanical gearbox
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163:Cooling system:
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99:reduction drive
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72:Mistral Engines
68:aircraft engine
52:Mistral Engines
37:National origin
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133:Displacement
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323:aeroengines
179:Performance
78:for use in
42:Switzerland
364:Categories
209:References
157:Fuel type:
151:Components
142:Dry weight
236:1368-485X
114:Data from
21:G-230-TS
349:G-360-TS
339:G-230-TS
261:28 March
192:See also
159:gasoline
234:
165:liquid
76:Geneva
344:G-300
334:G-200
126:Type:
116:Tacke
65:Swiss
63:is a
26:Type
263:2018
232:ISSN
59:The
74:of
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217:^
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312:e
305:t
298:v
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