12. The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems
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12. The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems |
| Loza A. V., Yelansky Y. A., Pokatayev V. N., Karzova А. А.
Yangel Yuzhnoye State Design Office, Dnipro, Ukraine |
| Kosm. teh. Raket. vooruž. 2016 (2); 75-79 |
| Language: Russian |
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Annotation:
Considered is the application of the thermoelectric cooling modules to enhance the operating reliability of the spacecraft’s temperature control system in the severe climatic conditions, schematic diagram of the thermoelectric cooling system is given.
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