Forming method of variable cross section special-shaped single tube of thrust chamber body of liquid-propellant rocket engine

The invention discloses a forming method of a variable cross section special-shaped single tube of a thrust chamber body of a liquid-propellant rocket engine. The method comprises the following stepsthat (1), bend shaping is conducted, specifically, a single tube workpiece in the annealing state and...

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Bibliographic Details
Main Authors DU LIYA, XIONG HEQIN, LI YULEI, LI JINTAO
Format Patent
LanguageChinese
English
Published 12.04.2019
Subjects
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