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Thermal Stores in Spacecraft Heating Systems

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Abstract

In the present work, we consider the use of thermal stores in spacecraft heating systems. The advantages and disadvantages of various approaches to heat storage are compared. The use of heat stores with a melting working material is most promising and practicable at present.

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Authors and Affiliations

  1. Moscow Aviation Institute, Moscow, Russia

    A. E. Belyavskii, S. V. Novikov, A. E. Sorokin & I. A. Shangin

Authors
  1. A. E. Belyavskii
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  2. S. V. Novikov
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  3. A. E. Sorokin
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  4. I. A. Shangin
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Corresponding author

Correspondence to A. E. Belyavskii.

Additional information

Translated by Bernard Gilbert

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Belyavskii, A.E., Novikov, S.V., Sorokin, A.E. et al. Thermal Stores in Spacecraft Heating Systems. Russ. Engin. Res. 39, 507–509 (2019). https://doi.org/10.3103/S1068798X19060078

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  • DOI: https://doi.org/10.3103/S1068798X19060078

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