OPTIMIZATION OF GALVANIC BATTERY DESIGN FOR SPACECRAFT
DOI:
https://doi.org/10.34185/1991-7848.itmm.2022.01.050Keywords:
heat loss, heating system, screen, insulation, batteries, heat transferAbstract
In accordance with the objectives of the research, modeling of the thermal state of the 24V power supply in the operating conditions of -40oC was performed. Two variants of thermostating are considered: on the basis of radioactive heating elements (RNE) and on the basis of autonomous resistive heating system.
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