Solid rocket engine extinguishing and cooling device

The invention, which relates to the technical field of rocket engines, discloses a solid rocket engine extinguishing and cooling device which comprises a rotating mechanism, a feeding mechanism, a spray gun mechanism and a pneumatic control system. An oscillating cylinder Q1 of the rotating mechanis...

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Bibliographische Detailangaben
Hauptverfasser: QIAN MING, WU JIAJIA, FANG JINGJING, CHEN JIAN, MAO KANKANG, QIANG KEJIE, ZHAO ZHIRU, SHEN JUNJIE
Format: Patent
Sprache:chi ; eng
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