Article

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Title

Thermal circuit of «Yubileyny» small class spacecraft and heat exchanger parameters determination

Authors

¹M.Z. Muradimov, ¹V.V. Dvirny, ¹G.V. Dvirny, ¹S.G. Kukushkin, ²V.V. Golovanova, ³E.S. Sidorova

Organizations

¹JCS «Academician M. F. Reshetnev» Information Satellite Systems»
Zheleznogorsk, Russia
²The Arsenal Design Bureau named after M. V. Frunze
St. Petersburg, Russia
³ Siberian Federal University
Krasnoyarsk, Russia

Abstract

Calculations of the heat exchanger (radiator) parameters of the group of temperature-control system in unpressurized small class telecommunication satellite (satellite mass < 600 kg), on low circular orbit - 1500 km, are shown.

Keywords

thermal circuit, calculation of radiator parameters, satellite «Yubileyny», «hot» and «cold» variant, inboard and off-board heat flow, energy balance

For citing this article

Muradimov M.Z., Dvirny V.V., Dvirny G.V., Kukushkin S.G., Golovanova V.V., Sidorova E.S. Thermal circuit of «Yubileyny» small class spacecraft and heat exchanger parameters determination // The Research of the Science City, 2015, no. 1, pp. 18-23.

This Article is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).