Thermal analysis of spacecraft propulsion system and its validation-Reference-Cited by-同舟云学术

Thermal analysis of spacecraft propulsion system and its validation

Published:2004-05 Issue:5 Volume:18 Page:847-856
ISSN:1226-4865
Container-title:KSME International Journal
language:en
Short-container-title:KSME International Journal

Author:

Han Cho Young,Choi Joon-Min

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF02990304.pdf

Reference13 articles.

1. Analytix Corporation. 1996a.AC/SINDA User’s Manual.

2. Analytix Corporation, 1996b.AC/TRASYS User’s Manual.

3. Choi, H. S., 1996. “An Analysis for the Sizing of PSAT Dual Thruster Module Heaters.”Proceedings of the 3rd Asia-Pacific Conference on Multilateral Cooperation In Space Technology and Applications, May 27-31, Seoul. Korea. pp. 466–471.

4. Gebhart. 1971.Heat Transfer, McGraw-Hill.

5. Gilmore, D. G., 1994.Satellite Thermal Control Handbook, The Aerospace Corporation Press EI Segundo, California.

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