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

Carbon

Volumn 48, Issue 3, 2010, Pages 924-925

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

^a AEROSPACE RESEARCH INSTITUTE OF MATERIALS AND PROCESSING TECHNOLOGY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

C/C COMPOSITES; CARBON/CARBON; HIGH THERMAL CONDUCTIVITY; HYPERSONIC AIRCRAFT; THERMAL BURDEN; THERMAL PROTECTION SYSTEM;

CARBON CARBON COMPOSITES; HEAT SHIELDING; HYPERSONIC VEHICLES; THERMAL INSULATING MATERIALS; THERMOANALYSIS;

THERMAL CONDUCTIVITY;

EID: 71649103001     PISSN: 00086223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.carbon.2009.10.043     Document Type: Letter

References (4)

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. Bowers D.A., Davis J.W., and Dinwiddie R.B. Development of 1-D carbon composites for plasma-facing components. J Nucl Mater 212-215 (1994) 1163-1167
3. Ting J.M., and Lake M.L. Vapor-grown carbon-fiber reinforced carbon composites. Carbon 33 5 (1995) 663-667
4. Liu Z.J., Guo Q.G., Shi J.L., Zhai G.T., and Liu L. Graphite blocks with high thermal conductivity derived from natural graphite flake. Carbon 46 (2008) 414-421