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Application of lightweight titanium alloy nozzle in LOX-LH2 rocket engine
(
PDF
)
《火箭推进》
[ISSN:
1672-9374
/CN:
CN 61-1436/V
]
Issue:
2016年04期
Page:
1-6
Research Field:
专论与综述
Publishing date:
Info
Title:
Application of lightweight titanium alloy nozzle in LOX-LH2 rocket engine
Author(s):
XU Xiaoyong
;
ZHAO Shihong
;
WANG Zhao
Keywords:
LOX-LH2 rocket engine
;
thrust chamber
;
titanium alloy nozzle
;
regenerative cooling
PACS:
V434-34
DOI:
-
Abstract:
-
References:
-
Memo
Memo:
-
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1900-01-01