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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Main Authors | , , , |
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Format | Patent |
Language | Chinese English |
Published |
12.04.2019
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Subjects | |
Online Access | Get full text |
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