Temperature Distribution in the Spherical Shell of a Gauge-Alignment Spacecraft
- Autores: Zarubin V.S.1, Zimin V.N.1, Kuvyrkin G.N.1
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Afiliações:
- Bauman Moscow State Technical University
- Edição: Volume 58, Nº 6 (2017)
- Páginas: 1083-1090
- Seção: Article
- URL: https://journals.rcsi.science/0021-8944/article/view/160500
- DOI: https://doi.org/10.1134/S0021894417060141
- ID: 160500
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Resumo
A thermal model for the aluminized polymer shell of a gauge-alignment spacecraft was developed to calculate the steady-state temperature distribution of this shell at a fixed orientation to the Sun. A modified version of the model was used to analyze the quasistationary distribution of the shell temperature in the case of its rotation with a constant angular velocity about an axis perpendicular the direction to the Sun.
Sobre autores
V. Zarubin
Bauman Moscow State Technical University
Autor responsável pela correspondência
Email: zarubin@bmstu.ru
Rússia, Moscow, 105005
V. Zimin
Bauman Moscow State Technical University
Email: zarubin@bmstu.ru
Rússia, Moscow, 105005
G. Kuvyrkin
Bauman Moscow State Technical University
Email: zarubin@bmstu.ru
Rússia, Moscow, 105005
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