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Selection of the Design Parameters for Heat Stores in Spacecraft Temperature Maintenance

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Abstract

A method is proposed for selecting the design parameters of heat stores used in spacecraft temperature maintenance. The position of the store in the system is chosen. The heat store’s design, geometric dimensions, thermal capacity, and working medium are determined.

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Authors and Affiliations

  1. Moscow Aviation Institute, Moscow, Russia

    A. E. Belyavskii

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  1. A. E. Belyavskii
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Correspondence to A. E. Belyavskii.

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Translated by B. Gilbert

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Belyavskii, A.E. Selection of the Design Parameters for Heat Stores in Spacecraft Temperature Maintenance. Russ. Engin. Res. 41, 745–747 (2021). https://doi.org/10.3103/S1068798X21080074

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  • DOI: https://doi.org/10.3103/S1068798X21080074

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