РАЗРАБОТКА КОНЦЕПЦИИ ДВУХФАЗНОЙ СИСТЕМЫ ТЕПЛООТВОДА СПУТНИКА
For spacecraft (SC) with power unit capacity more than 4 ... 6 kW promising construction of thermal control system (TCS) based on two-phase mechanically pumped loops (2PMPL). The development of 2PMPL has been carried out quite intensively since the early '80s. However, so far there are no examp...
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| Published in: | Avìacìjno-kosmìčna tehnìka ì tehnologìâ no. 1; pp. 31 - 46 |
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| Main Author: | |
| Format: | Journal Article |
| Language: | English |
| Published: |
26.02.2021
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| ISSN: | 1727-7337, 2663-2217 |
| Online Access: | Get full text |
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