Atomic oxygen resistant protective coatings for the Hubble Space Telescope solar array in low earth orbitThe Hubble Space Telescope back-up solar array (BSFR-ATOX) was designed with atomic oxygen resistant materials to replace the original high efficiency cell (HEC) array. Pending qualification of the BSFR-ATOX array, protective coatings for application to the existing HEC array were evaluated. Three polysiloxane-type coating materials, SWS V-10, DC-100, and CV-1144 were evaluated with respect to atomic oxygen resistance, outgassing, contamination potential, stability under UV irradiation, electron-proton irradiation, thermal cycling, and long-term storage after application. Atomic oxygen testing included characterization of the atomic oxygen plasma using comparison of Kapton reaction to existing flight data, residual gas analysis, and temperature measurements. Results from these tests show DC-100 as a greater contamination concern if used in the vicinity of sensitive optical surfaces, i.e., solar cell cover glasses. The SWS V-10 and CV-1144 coatings met all acceptance criteria.
Document ID
19910056895
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Burns, H. D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Whitaker, A. F. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Linton, R. C. (NASA Marshall Space Flight Center Huntsville, AL, United States)