TitleApplication of heat-exchangeunits in binary return system for technology ground work developing of spacecraft
Authors1G.V. Dmitriev, 1O.V. Shilkin, 1A.P. Kolesnikov, 1V.V. Dvirny, 2E.S. Sidorova
Organizations1JCS «Academician M.F. Reshetnev» Information Satellite Systems»
2Siberian Federal University
AbstractAn on-board binary return system module, which is used as thermal control chamber instrument for technology ground work developing of spacecraft, has been developed. We provide the analysis of the specification of the binary return system module. We present the advantages of mechanical pump-based temperature control chamber for heat transfer fluid injection by means of binary return system module versus the single-phase module.
KeywordsBinary return system, technology ground work, on-board binary return system module, temperature control chamber for spacecraft, temperature control, compressor station, vapor generator, hydro accumulator, electromechanical pump
For citing this articleDmitriev G.V., Shilkin O.V., Kolesnikov A.P., Dvirny V.V., Sidorova E.S. Application of heat-exchangeunits in binary return system for technology ground work developing of spacecraft // The Research of the Science City, 2014, no. 4, pp. 21-27.
This Article is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).