On the issue of prospective hybrid rocket engine with the ability of deep adjustment
Автор: Kartashev A.L., Shulev I.S.
Рубрика: Расчет и конструирование
Статья в выпуске: 33 (292), 2012 года.
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This article presents a description of a new hybrid rocket engine that is going to patented in the Russian Federation (patent application for “Hybrid rocket engine” data 02.07.2012 № 2012128309).
Hybrid rocket engine, solid rocket engine, spacecraft, specific impulse of burn, deep adjustment, liquid-propellant rocket engine
Короткий адрес: https://sciup.org/147151588
IDR: 147151588
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