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A multidisciplinary design optimization approach for a regeneratively cooled thrust chamber(PDF)

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

Issue:
2005年02期
Page:
12-16
Research Field:
Publishing date:

Info

Title:
A multidisciplinary design optimization approach for a regeneratively cooled thrust chamber
Author(s):
Fang Jie;  Cai Guobiao;  2 Wang Jue;  Chen Jun
1School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China 2Institute of Beijing Aerospace Power Mechanics, Beijing 100076, China
Keywords:
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PACS:
V432
DOI:
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Abstract:
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References:

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Memo

Memo:
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Last Update: 1900-01-01