Calculations for stress-strained state of a panel of a solar array under thermal loading conditions

Heading: 
Space Materials and Technologies
1Xiaoyan, Wang, 2Pokhyl, Yu.A, Koval', KV, 1Shiyu, He., 3Gavrylov, RV
1Center for Space Materials Science and Simulation of the Cosmic Factors of the Harbin Polytechnic University, Harbin, China
2B.I. Verkin Institute for Low Temperature Physics and Engineering, NAS of Ukraine, Kharkiv, Ukraine
3B.Verkin Institute for Low Temperature Physics and Engineering of the National Academy of Sciences of Ukraine, Kharkiv, Ukraine
Kosm. nauka tehnol. 2005, 11 ;(5-6):103-110
https://doi.org/10.15407/knit2005.05.103
Publication Language: Russian
Abstract: 
We developed two unified analytical methods for stress-strained state (SSS) determination of panels of solar arrays of spacecrafts at thermal loading. A determination and an analysis of SSS for solar array testing model are made and the results of the analysis are compared with ones from the finite element method. Some recommendations for panel optimal structure determination are developed on the basis of our parametrical investigation.
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References: 
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