THE ANALYSIS OF THE HEAT CONTROL ACCUMULATOR VOLUME IMPACT ON THE OPERABILITY OF TWO-PHASE HEAT TRANSFER LOOP OF A SPACECRAFT THERMAL CONTROL SYSTEM
The world trend in the development of space vehicles is the expansion of their functionality, which leads to an increase in the power consumption, most of which is allocated in the elements of spacecraft equipment in the form of heat. To remove heat from the equipment elements, transfer it to the he...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
National Aerospace University «Kharkiv Aviation Institute»
2018-12-01
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| Series: | Авіаційно-космічна техніка та технологія |
| Subjects: | |
| Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/546 |