Investigation into tolerance of polysiloxane-block-polyimide film against atomic oxygen

Author:

Miyazaki Eiji,Tagawa Masahito,Yokota Kumiko,Yokota Rikio,Kimoto Yugo,Ishizawa Junichiro

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference10 articles.

1. F.W. Crossman, Spacecraft material applications—long-term stability questions, NASA-CP-2269, NASA, 1982.

2. Atomic oxygen and its effects of materials;Tennyson,1993

3. K.A. Smith, Evaluation of oxygen interaction with materials (EOIM)—STS-8 atomic oxygen effects, AIAA-85-7021, American Institute of Aeronautics and Astronautics, 1985, pp. 190–197.

4. J. Ishizawa, K. Mori, F. Imai, I. Yamagata, M. Suzuki, Results of the space-environment exposure experiment SM/MPAC&SEED on the International Space Station (2): siloxane coated polyimide films, and silicone based paints and adhesives, in: Proceedings of the 10th International Symposium on Materials in a Space Environment (CD-ROM), ESA-SP-616, European Space Agency, 2006.

5. Study of surface chemical changes and erosion rates for CV-1144-0 silicone under electron cyclotron resonance oxygen plasma exposure;Yan;J. Vac. Sci. Technol.,2001

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