Effects of Thermal Cycling on Atomic Oxygen Interaction with Graphite/Cyanate Composite

Author:

Zhai Ruiqiong,Liu Yuming,Tian Dongbo,Jiang Haifu,Li Yuting

Publisher

Springer International Publishing

Reference14 articles.

1. Jiang L, He S, Yang S et al (2001) Application of carbon (graphite) fiber/epoxy composites in the spacecraft and the research on their behavior [J]. J Mater Eng 9:39–43

2. Silverman EM (1996) Space environment effects on spacecraft: LEO materials selection guide. NASA contractor report 4661 [R]

3. Tang J (2010) Review of studies of carbon fiber resin matrix composites [J]. Spacecr Environ Eng 27(3):269–2804

4. Huang B, Tong J (2010) Space environment engineering [M]. China Science and Technology Press, Beijing, pp 3–8

5. Zhao S, Shen Z, Xing Y et al (2002) Experimental investigations of atomic oxygen effects on a carbon fiber/epoxy resin composite material [J]. J Beijing Univ Aeronaut Astronaut 28(6):668–670

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