Article

Cover

Title

Application of heat-exchangeunits in binary return system for technology ground work developing of spacecraft

Authors

¹G.V. Dmitriev, ¹O.V. Shilkin, ¹A.P. Kolesnikov, ¹V.V. Dvirny, ²E.S. Sidorova

Organizations

¹JCS «Academician M.F. Reshetnev» Information Satellite Systems»
Zheleznogorsk, Russia
²Siberian Federal University
Krasnoyarsk, Russia

Abstract

An 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.

Keywords

Binary 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 article

Dmitriev 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).