DETERMINATION OF THE CONVECTIVE HEAT TRANSFER COEFFICIENT IN A HEAT CONTROLLED ACCUMULATOR FOR THE CONDITIONS OF WEIGHTLESS

In the modern world with the increasing power of spacecraft heat dissipation, the need has arisen to use efficient heat removal systems with two-phase heat transfer contours. Their advantages are determined by the fact that they can carry a much larger amount of heat per unit of consumption than whe...

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Bibliographic Details
Main Authors: Полина Сергеевна Коваль, Эдем Русланович Решитов, Рустем Юсуфович Турна
Format: Article
Language:English
Published: National Aerospace University «Kharkiv Aviation Institute» 2019-08-01
Series:Авіаційно-космічна техніка та технологія
Subjects:
Online Access:http://nti.khai.edu/ojs/index.php/aktt/article/view/859