高导热沥青基碳纤维复合材料在航天器中的应用现状及展望

doi:10.11896/cldb.22080244

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Abstract With the development of the new generation of spacecraft towards the direction of super-large, micro-miniaturization and high-efficiency, the demand for lightweight, high-strength, high modulus and high thermal conductivity materials for spacecraft is increasingly urgent. Compared with traditional PAN-based carbon fiber, high thermal conductivity pitch-based carbon fiber has ultra-high thermal conductivity, higher tensile modulus and lower thermal expansion coefficient. High thermal conductivity pitch-based carbon fiber is an ideal material to realize the functional integration of load bearing, heat transfer and thermal dimensional stability. It has been widely used in the aerospace field and has shown great application prospects. This paper introduces the performance characteristics, development status and application status of high thermal conductivity pitch-based carbon fiber and its composites in spacecraft. The application status of high thermal conductivity pitch-based carbon fiber composites in spacecraft thermal management structure, thermal protection structure, high dimensional stability structure, multi-function structure and electronic equipment shell are reviewed. Finally, the development and application prospects of high thermal conductivity pitch-based carbon fiber composites are prospected.

Key words： high thermal conductivity high modulus pitch-based carbon fiber thermal management high dimensional stability multifunctional structure

Published: Online: 2024-01-16

CLC number:

TB332

Fund:Rapid Transformation Project of Equipment Development Department(8091C29).

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	Articles by authors
	YANG Qiang
	LIU Hongxin
	HE Duanpeng
	CHEN Haifeng
	CHEN Weiqiang
	JIN Jing
	PAN Fuming

Cite this article:

YANG Qiang,LIU Hongxin,HE Duanpeng, et al. Application Status and Prospect of High Thermal Conductivity Pitch-based Carbon Fiber Composites in Spacecraft[J]. Materials Reports, 2024, 38(1): 22080244-8.

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http://www.mater-rep.com/EN/10.11896/cldb.22080244 OR http://www.mater-rep.com/EN/Y2024/V38/I1/22080244

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