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Dushkin S-155 : ウィキペディア英語版 | Dushkin S-155
The Dushkin S-155 was a liquid-fueled rocket motor designed by Leonid Dushkin specifically for use in the Mikoyan-Gurevich Ye-50 and Ye-50A (aka MiG-23U) experimental-developmental aircraft in the 1950s. It delivered 37.3 kN (8380 lbf) and ran on a mix of TG-02 hypergolic kerosene and AK-20 oxidizer (nitric acid). The fuel pumps were powered with grade T hydrogen peroxide.〔Gordon, Yefim "MiG-21" ISBN 978-1-85780-257-3〕 ==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「Dushkin S-155」の詳細全文を読む
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