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The engine is a twin-rotor, 2X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline
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98:with a reduction ratio of 2.82:1. It employs dual
227:, pages 260-261. Flying Pages Europe SARL, 2015.
102:systems and produces 150 hp (112 kW).
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94:design, with an integral mechanical gearbox
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225:World Directory of Light Aviation 2015-16
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134:2X3X654 cc (39.9 cu in)
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223:Tacke, Willi; Marino Boric; et al:
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125:Twin rotor Wankel aircraft engine
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171:integral mechanical gearbox
143:132 kg (291.0 lb)
70:, designed and produced by
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184:150 hp (112 kW)
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343:Pistonless rotary engine
338:Mistral aircraft engines
200:List of aircraft engines
117:General characteristics
106:Specifications (G-200)
86:Design and development
100:electronic ignition
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160:Cooling system:
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96:reduction drive
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72:Mistral Engines
68:aircraft engine
52:Mistral Engines
37:National origin
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176:Performance
78:for use in
42:Switzerland
332:Categories
206:References
154:Fuel type:
148:Components
139:Dry weight
233:1368-485X
111:Data from
317:G-360-TS
307:G-230-TS
189:See also
156:gasoline
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162:liquid
76:Geneva
21:G-200
312:G-300
302:G-200
123:Type:
113:Tacke
65:Swiss
63:is a
26:Type
229:ISSN
59:The
74:of
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214:^
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280:e
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266:v
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