Problems and the outlook for the development of effective systems of controlling the thermal regimes of spacecraft are considered. The process of creating and using the apparatus of mathematical modeling for the purpose of comparing the energy characteristics of different systems is described. The characteristics of forward and reverse working cycles of two-phase closed systems that control the thermal regimes are compared.
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Translated from Khimicheskoe i Neftegazovoe Mashinostroenie, No. 10, pp. 45–48, October, 2015.
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Delkov, A.V., Kishkin, A.A., Lavrov, N.A. et al. Analysis of Efficiency of Systems for Control of the Thermal Regime of Spacecraft. Chem Petrol Eng 51, 714–719 (2016). https://doi.org/10.1007/s10556-016-0110-z
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DOI: https://doi.org/10.1007/s10556-016-0110-z