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Rocket turbine engine : ウィキペディア英語版 | Rocket turbine engine A rocket turbine engine is a combination of two types of propulsion engines: a liquid fuel rocket and a turbine jet engine. Its power-to-weight ratio is a little higher than a regular jet engine. and work at higher altitudes. 〔"Analysis of the effect of factors on the efficiency of liquid rocket turbine" by Zu, Guojun; Zhang, Yuanjun ''Journal of Propulsion Technology '' no. 6, p. 38-43, 58.()〕 〔 Hydrogen peroxide based propulsion system for micro air vehicle applications b WS Cheung, JR Tilston ISABE 99-7298 ()〕 〔"Testing of a novel propulsion system for micro air vehicles" ''Pfoceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering" Volume 215, Number 4, pages 207-218 / 2001 () 〕 ==References==
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「Rocket turbine engine」の詳細全文を読む
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