Temperature Distribution in the Spherical Shell of a Gauge-Alignment Spacecraft


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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.

作者简介

V. Zarubin

Bauman Moscow State Technical University

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Email: zarubin@bmstu.ru
俄罗斯联邦, Moscow, 105005

V. Zimin

Bauman Moscow State Technical University

Email: zarubin@bmstu.ru
俄罗斯联邦, Moscow, 105005

G. Kuvyrkin

Bauman Moscow State Technical University

Email: zarubin@bmstu.ru
俄罗斯联邦, Moscow, 105005

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