Application of high temperature heat pipe in hypersonic vehicles thermal protection-Reference-Cited by-同舟云学术

Application of high temperature heat pipe in hypersonic vehicles thermal protection

Published:2011-07-10 Issue:4 Volume:18 Page:1278-1284
ISSN:1005-9784
Container-title:Journal of Central South University of Technology
language:en
Short-container-title:J. Cent. South Univ. Technol.

Author:

Bai Tong,Zhang Hong,Xu Hui

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://link.springer.com/content/pdf/10.1007/s11771-011-0833-0.pdf

Reference21 articles.

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2. HOU Yu-zhu, ZHENG Jing-liang, DONG Wei. Transient test of aerodynamic heating for hypersonic vehicle [J]. Journal of Aerospace Power, 2010, 25(2): 343–347.

3. LIU Shuang, ZHANG Bo-ming. Experimental study on a transpiration cooling thermal protection system [J]. Science China Technological Sciences, 2010, 53(10): 2765–2771. (in Chinese)

4. MARCOS J, COLETO J, ADARRAGA O. Smart thermal protection systems [C]// 59th International Astronautical Congress. Pairs: IAF, 2008: 5669–5677.

5. BOLIVAR C M V, ANTONINI A, BIAMINO S, PAVESE M, FINO P, BADINI C. Oxidation resistance of multilayer SiC for space vehicle thermal protection systems [J]. Advanced Engineering Materials, 2010, 12(7): 617–622.

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