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Radiation Damage Effects on Spacecraft Materials

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Part of the book series: NATO ASI Series ((NSSE,volume 245))

Abstract

In geostationary orbit satellite materials are subject to radiation damage caused by trapped protons and electrons. This paper describes radiation damage testing carried out on novel imide — based conductive coatings applied to Kapton and glass. As background information, the radiation test facilities themselves are described, with a discussion of the relationship between the test conditions and the effects of the near earth orbit environment.

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References

  1. Chapiro, A. (Ed.), “Radiation Chemistry of Polymeric Systems”, Interscience, New York. (Volume XV in the High Polymers monograph series), 1962.

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  2. Verdin, D. and Duck, J.J., “Surface Modifications to Minimise the Electrostatic Charging of Kapton in the Space Environment”, J. of Electrostatics, 20, 123–129, 1987.

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  3. Data taken from “The radiation design handbook” ESA PSS-01-609 European Space Agency, Noordwijk, The Netherlands, 1990 (draft).

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  4. Janni, J.F., “Calculations of energy loss, range, pathlength, straggling, multiple scattering, and the probability of inelastic nuclear collisions for 0.1 to 1000 MeV protons”, report AFWL-TR 65- 150, 1966.

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© 1993 Springer Science+Business Media Dordrecht

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Walters, W.S. (1993). Radiation Damage Effects on Spacecraft Materials. In: DeWitt, R.N., Duston, D., Hyder, A.K. (eds) The Behavior of Systems in the Space Environment. NATO ASI Series, vol 245. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-2048-7_35

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  • DOI: https://doi.org/10.1007/978-94-011-2048-7_35

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-010-4907-8

  • Online ISBN: 978-94-011-2048-7

  • eBook Packages: Springer Book Archive

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