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Mathematical simulation of heat exchange in a nonhermetic instrumental compartment of a spacecraft

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Abstract

We present physical and dynamic thermal mathematical models in distributed and lumped parameters, calculation algorithms, software, and some results of numerical calculations of radiative-conductive heat exchange in blocks and modules carrying thermally loaded on-board equipment in a nonhermetic instrumental compartment of a proposed durable communication spacecraft with improved mass, size, and energy characteristics improved in comparison with traditional hermetic compartments.

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Authors and Affiliations

  1. Scientific Research Institute of Applied Mathematics and Mechanics at the Tomsk State University, Tomsk, Russia

    V. A. Burakov, E. N. Korchagin, V. P. Kozhukhov, A. S. Tkachenko & I. V. Shcherbakov

  2. M. F. Reshetnev Science and Production Association of Applied Mechanics, USSR

    V. A. Burakov, E. N. Korchagin, V. P. Kozhukhov, A. S. Tkachenko & I. V. Shcherbakov

Authors
  1. V. A. Burakov
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  2. E. N. Korchagin
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  3. V. P. Kozhukhov
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  4. A. S. Tkachenko
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  5. I. V. Shcherbakov
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 73, No. 1, pp. 113–124, January–February, 2000.

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Burakov, V.A., Korchagin, E.N., Kozhukhov, V.P. et al. Mathematical simulation of heat exchange in a nonhermetic instrumental compartment of a spacecraft. J Eng Phys Thermophys 73, 112–123 (2000). https://doi.org/10.1007/BF02681685

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  • DOI: https://doi.org/10.1007/BF02681685

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