Improvement of Stiffness Properties of Spacecraft Solar Panels
- Authors: Khmel’nitskii Y.A.1, Salina M.S.2
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Affiliations:
- Romashin ONPP Tekhnologiya
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 2 (2018)
- Pages: 304-306
- Section: Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230547
- DOI: https://doi.org/10.3103/S1068799818020228
- ID: 230547
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Abstract
This paper considers changes in design of solar panels due to a need to improve reliability and to increase the service life.
Keywords
About the authors
Ya. A. Khmel’nitskii
Romashin ONPP Tekhnologiya
Email: 2707fm@mail.ru
Russian Federation, Kievskoe sh. 15, Obninsk, Kaluzhskaya oblast, 249031
M. S. Salina
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: 2707fm@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
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