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Pressure variation mechanism of filled propellant tank for attitude control engine(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2005年05期
Page:
19-21
Research Field:
Publishing date:

Info

Title:
Pressure variation mechanism of filled propellant tank for attitude control engine
Author(s):
1Pang Jianguo;  1Liu Xiaoping;  1Shao Yongping; 2Guo Fengmei
1Taiyuan Satellite Launch Center, Taiyuan 030027, China; 2China Academy of Launch Vehicle Technology, Beijing 100076, China
Keywords:
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PACS:
V434.23;
DOI:
-
Abstract:
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References:

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Memo

Memo:
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Last Update: 1900-01-01