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Heating of Components in the International Space Station

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Abstract

A thermal model of the International Space Station is proposed and used to calculate the total heat fluxes, by stochastic Monte Carlo modeling. The total heat fluxes consist of solar radiation, the infrared flux reflected from the Earth, and the infrared flux due to radiant heat transfer among the components of the station. On the basis of appropriate boundary conditions, the mean mass temperatures and limiting temperature difference typical of the given orbit are determined.

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Authors and Affiliations

  1. Moscow Aviation Institute, Moscow, Russia

    N. O. Borshchev, A. E. Belyavskii & A. E. Sorokin

Authors
  1. N. O. Borshchev
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  2. A. E. Belyavskii
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  3. A. E. Sorokin
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Corresponding authors

Correspondence to N. O. Borshchev, A. E. Belyavskii or A. E. Sorokin.

Additional information

Translated by B. Gilbert

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Borshchev, N.O., Belyavskii, A.E. & Sorokin, A.E. Heating of Components in the International Space Station. Russ. Engin. Res. 40, 1141–1143 (2020). https://doi.org/10.3103/S1068798X20120291

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  • DOI: https://doi.org/10.3103/S1068798X20120291

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