Application of heat-exchangeunits in binary return system for technology ground work developing of spaсecraft
Автор: Dmitriev G.V., Shilkin O.V., Kolesnikov A.P., Dvirny V.V., Sidorova E.S.
Журнал: Космические аппараты и технологии.
Рубрика: Космонавтика
Статья в выпуске: 4 (10), 2014 года.
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Anon-board binary return system module, which is used as thermal control chamberinstrument for technology ground work developing of spacecraft, has beendeveloped. We provide the analysis of the specification of the binary returnsystem module. We present the advantages of mechanical pump-based temperaturecontrol chamber for heat transfer fluid injection by means of binary returnsystem module versus the single-phase module.
Binary return system, on-board binaryreturnsystem module, temperature control chamber for spacecraft, temperature control, compressor station, vapor generator, hydro accumulator, electromechanical pump, technology ground work
Короткий адрес: https://sciup.org/14117331
IDR: 14117331