Journal of Applied Mechanics and Technical Physics

, Volume 58, Issue 6, pp 1083–1090 | Cite as

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

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Abstract

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.

Keywords

spacecraft spherical shell equilibrium temperature quasistationary temperature distribution 
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Copyright information

© Pleiades Publishing, Ltd. 2017

Authors and Affiliations

  1. 1.Bauman Moscow State Technical UniversityMoscowRussia

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