Degradation of Solar Array Components in a Combined UV/VUV High Temperature Test Environment

Christel Nömayr; Claus Zimmermann; Premysl Janik; Christopher Semprimoschnig

doi:10.1051/e3sconf/20171604007

All issues

Volume 16 (2017)

E3S Web Conf., 16 (2017) 04007

References

Open Access

Issue		E3S Web Conf. Volume 16, 2017 11^th European Space Power Conference


Article Number		04007
Number of page(s)		6
Section		Power Generation: Solar Generators Mission Design
DOI		https://doi.org/10.1051/e3sconf/20171604007
Published online		23 May 2017

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[1] Hall D.F. et al, Photo-Enhanced Spacecraft Contamination Deposition, AIAA 20th Thermophysics Conference, AIAA-85-0953, 1985. [Google Scholar]

[2] Stewart T.B. et al, Photochemical Spacecraft Self-Contamination: Laboratory Results and Systems Impacts, AIAA Thermophysics, Plasmadynamics and Lasers Conference, AIAA-88-2728, 1988. [Google Scholar]

[3] Löhberg A. et al, The BepiColombo mercury planetary orbiter (MPO) solar array design, major developments and qualification, this conference [Google Scholar]

[4] Oberhüttinger C. et al, Simulating large area, high intensity AM0 illumination - test results from BepiColombo and Solar Orbiter qualification, this conference [Google Scholar]

[5] Poinas P., SOHO OSR degradation 11 years of flight data, report TEC-MCT/2008/3635/ln/PP [Google Scholar]