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Materials Testing Activities within ESA in Support of Future Inner Solar System Missions

Published online by Cambridge University Press:  01 February 2011

Christopher O. A. Semprimoschnig
Affiliation:
Materials Physics and Chemistry Section European Space Research and Technology Centre (ESTEC), European Space Agency (ESA), Keplerlaan 1, PO Box 299, NL-2200 AG Noordwijk, The Netherlands
Stan Heltzel*
Affiliation:
Materials Physics and Chemistry Section European Space Research and Technology Centre (ESTEC), European Space Agency (ESA), Keplerlaan 1, PO Box 299, NL-2200 AG Noordwijk, The Netherlands
Marc van Eesbeek*
Affiliation:
Materials Physics and Chemistry Section European Space Research and Technology Centre (ESTEC), European Space Agency (ESA), Keplerlaan 1, PO Box 299, NL-2200 AG Noordwijk, The Netherlands
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Abstract

In this paper the ESA internal approach regarding the assessment of materials for inner solar system missions is presented. A main part of the work is devoted to the assessment of thermal control materials and space environmental testing at elevated temperature. As these materials are the most exposed it is important to understand how they will interact with the relevant space environment at elevated temperature. Driving parameters for materials degradation are discussed and on-going testing efforts are described. An important input parameter for thermal models is the knowledge of the end of life values for the thermo-optical properties as these determine the equilibrium temperatures. In certain cases end of life testing needs to be done when the uncertainty of extrapolation is too high.

Type
Research Article
Copyright
Copyright © Materials Research Society 2005

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References

5. References

[1] Stramaccioni, D., “Mercury Environmental Specification” (Part 1 ), issue 2, ESA/ESTEC 2002 Google Scholar
[2] Sorensen, J. & Evans, H., “Mercury Environmental Specification” (Part 2), issue 2, ESA/ESTEC 2002 Google Scholar
[3] Moser, M., Heltzel, S., Semprimoschnig, C.O.A., “SCREENING OF THE THERMAL ENDURANCE OF SPAC E MATERIALS BY KINETIC MODELLING, MRS 2004, Fall Meeting, Boston, USA Google Scholar
[4] Yokota, R., “ Recent trends and space applications of polyimides ”, J. of Photopolymer Sc & Techn., Vol 12, 2, 209, 1999 Google Scholar
[5] Traeger, R. and Salazar, E., “Thermal Aging of polyimide films”, Polym Preprints 12, 292 (1971)Google Scholar
[6] Matsumoto, T, “Nonaromatic polyimides derived from cycloaliphatic monomers, Macromolecules, 32, 4933, 1999 Google Scholar
[7] Hasegawa, M., Sensui, N., Shindo, Y., Yokota, R., “ Structure and properties of novel asymmetric biphenyl type polyimides. Homo and copolymers and blends , Macromolecules, 32, 387, 1999 Google Scholar
[8] Russell, D.A., Fogdall, L.B., Bohnhoff- Hlavacek, G., ‘Simulated space environmental testing on thin films”, NASA/CR-2000–210101, April 2000 Google Scholar
[9] Iwata, M., Tohyama, F., Ohnisi, A., Hirosawa, H., Shimazaki, K., “Evaluation of New Thermal Control Material for Inner Planetary Missions, SAE Paper 981686, 1998 Google Scholar
[10] Heltzel, S., Semprimoschnig, C.O.A., High Performance Polymers, Vol. 16, No. 2, 235248 (2004)Google Scholar
[11] ESA ECSS 70 09, ESA/ESTEC, Noordwijk, The Netherlands, August 2003 Google Scholar
[12] Semprimoschnig, C.O.A., Heltzel, S., Polsak, A., Eesbeek, M.v., High Performance Polymers, Vol. 16, No. 2, 207220 (2004)Google Scholar