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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Bibliographic Details
Main Authors: Artem Hodunov, Gennady Gorbenko, Pavel Gakal
Format: Article
Language:English
Published: National Aerospace University «Kharkiv Aviation Institute» 2021-10-01
Series:Авіаційно-космічна техніка та технологія
Subjects:
Online Access:http://nti.khai.edu/ojs/index.php/aktt/article/view/1544