Application of a high thermal conductivity C/C composite in a heat-redistribution thermal protection system-Reference-Cited by-同舟云学术

Application of a high thermal conductivity C/C composite in a heat-redistribution thermal protection system

Published:2010-03 Issue:3 Volume:48 Page:924-925
ISSN:0008-6223
Container-title:Carbon
language:en
Short-container-title:Carbon

Author:

Li Tong-Qi,Xu Zheng-Hui,Hu Zi-Jun,Yang Xiao-Guang

Funder

State Key Development Program (973) for Basic Research of China

Science and Technology Basic Research of Chinese National Defence Industry

Publisher

Elsevier BV

Subject

General Chemistry,General Materials Science

Reference4 articles.

1. Ai BC, Mao GL, Jiang GQ. Heat-redistribution thermal protection mechanism of hypersonic aircraft. In: 59th International astronautical congress. Glasgow, Scotland: The British Interplanetary Society; 2008. p. 242.

2. Development of 1-D carbon composites for plasma-facing components;Bowers;J Nucl Mater,1994

3. Vapor-grown carbon-fiber reinforced carbon composites;Ting;Carbon,1995

4. Graphite blocks with high thermal conductivity derived from natural graphite flake;Liu;Carbon,2008

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