The calculation of the heat control accumulator volume of two-phase heat transfer loop of a spacecraft thermal control system
Spacecraft thermal control systems based on two-phase mechanically pumped loops have advantages in terms of mass and power consumption for auxiliary needs compared to single-phase thermal control systems. However, the disadvantage of two-phase mechanically pumped loops is that when changing the heat...
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| Main Authors: | , , |
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| Format: | article |
| Language: | EN RU UK |
| Published: |
National Aerospace University «Kharkiv Aviation Institute»
2021
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| Subjects: | |
| Online Access: | https://doaj.org/article/fb28130972eb4717be30b770fa752bf2 |
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