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__NOTOC__ The Mistral G-300 is a Wankel rotary engine being developed by the Mistral Engine Company for use in light aircraft and helicopters. It is currently being readied for certification by the United States FAA. ==Design details== The G-300 uses gasoline as fuel. A similar design using kerosene or jet fuel is concurrently under development. It will be designated the K-300. The G-300 uses three rotating combustion chambers. It uses a liquid-cooling system, full electronic control (dubbed ''Digital Engine Management'' or DEM), and engine speed is reduced (2.8235:1) through a front-mounted planetary reduction drive. Maximum output speed is 2,300 revolutions/minute. In normally aspirated configuration the G-300 is rated at 300 hp (224 kW). With optional turbocharging it is rated at 360 hp (269 kW). 抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Mistral G-300」の詳細全文を読む スポンサード リンク
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