Publication Date:
2019-07-13
Description:
Various candidate solar panel designs were evaluated, both theoretically and experimentally, with respect to their thermal cycling survival capability, and in particular with respect to an accelerated simulation of thermal cycles representative of Viking '75 mission requirements. The experimental results were obtained on 'mini-panels' thermally cycled in a newly installed automated test facility herein described. The resulting damage was analyzed physically and theoretically, and on the basis of these analyses the panel design was suitably modified to significantly improve its ability to withstand the thermal environment. These successful modifications demonstrate the value of the complementary theoretical-experimental approach adopted, and discussed in detail in this paper.
Keywords:
SPACECRAFT PROPULSION AND POWER
Type:
Photovoltaic Specialists Conference; Nov 15, 1976 - Nov 18, 1976; Baton Rouge, LA
Format:
text
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