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	The performance characterization of carbon fiberreinforced plastic for space applications
	B. Sun; C. Xue; W. Shang; M. An; H. Zhao and H. Zhang
	2022
ISSN号	7316844
DOI	10.1177/07316844221141367
英文摘要	In this paper, the excellent dimensional stability and vacuum outgassing of high-performance carbon fiberreinforced plastic (CFRP) were discussed. First, the high-performance resin matrix was obtained by modifying cyanate resin, and the modified cyanate ester was used to make prepreg and laminates. Then, the mechanical property retention rate of laminates reached 90.79% under proton and electron irradiation. The average values of total mass loss and collected volatile condensable material of high-performance CFRP were 0.116% and 0.008%, respectively. Finally, the candidate tube and frame were fabricated based on the ply lay-up design. The candidate tube and frame were subjected to a series of experiments of thermal deformation and hygroscopic deformation to verify the dimensional stability. The thermal deformations of the tube and frame reached 0.468m/m and 4.579m/m, respectively, with a temperature variation of 4C. The measured hygroscopic deformation of the tube reached 8.16m/m in nearly 3months. The experimental results show that the high-performance CFRP can be used for precision optical structures of space telescopes. The Author(s) 2022.
URL标识	查看原文
内容类型	期刊论文
源URL	[http://ir.ciomp.ac.cn/handle/181722/66977]
专题	中国科学院长春光学精密机械与物理研究所
推荐引用方式 GB/T 7714	B. Sun,C. Xue,W. Shang,et al. The performance characterization of carbon fiberreinforced plastic for space applications[J],2022.
APA	B. Sun,C. Xue,W. Shang,M. An,&H. Zhao and H. Zhang.(2022).The performance characterization of carbon fiberreinforced plastic for space applications..
MLA	B. Sun,et al."The performance characterization of carbon fiberreinforced plastic for space applications".(2022).

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