Abstract
A mathematical model is developed for a radiant heat exchanger based on a two-layer hybrid structure for the thermal regulation systems of spacecraft. Hybrid radiant heat exchangers with a one-sided radiant panel surface are modeled. Such a heat exchanger is analyzed.
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Translated by B. Gilbert
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Belyavskii, A.E., Kudryavtseva, N.S., Sorokin, A.E. et al. Efficiency of Hybrid Radiant Heat Exchanger. Russ. Engin. Res. 42, 942–944 (2022). https://doi.org/10.3103/S1068798X22090040
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DOI: https://doi.org/10.3103/S1068798X22090040