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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Autores principales: Artem Hodunov, Gennady Gorbenko, Pavel Gakal
Formato: article
Lenguaje:EN
RU
UK
Publicado: National Aerospace University «Kharkiv Aviation Institute» 2021
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Acceso en línea:https://doaj.org/article/fb28130972eb4717be30b770fa752bf2
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