Mechanical characteristics of major components of solar arrays
Heading:
| 1Pokhyl, Yu.A, 2Gavrylov, RV, 1Yakovenko, LF, 1Aleksenko, EN, 1Lototskaya, VA, 3Xiaoyan, Wang, 3Shiyu, He., 4Tarasov, GV, 5Rassamakin, BM 1B.I. Verkin Institute for Low Temperature Physics and Engineering, NAS of Ukraine, Kharkiv, Ukraine 2B.Verkin Institute for Low Temperature Physics and Engineering of the National Academy of Sciences of Ukraine, Kharkiv, Ukraine 3Center for Space Materials Science and Simulation of the Cosmic Factors of the Harbin Polytechnic University, Harbin, China 4Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine 5National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”, Kyiv, Ukraine |
| Kosm. nauka tehnol. 2006, 12 ;(4):024-032 |
| https://doi.org/10.15407/knit2006.04.024 |
| Publication Language: Russian |
Abstract: We give some results of investigation of temperature influence, within 373 К to 77 К interval, on static and dynamic mechanical properties of structure materials to Ье employed with solar arrays of space vehicles. The experimental data thus oЬtained сап Ье used in further theoretical calculations for lifetime of solar arrays under conditions of influence Ьу multiple periodical thermal loads, in the course of orbltal flight.
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| Keywords: dynamic properties, solar arrays, structure materials |
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