350 rub
Journal Science Intensive Technologies №9 for 2014 г.
Article in number:
Mathematical hydraulic model of the combined thermal control systems of the spacecraft
Keywords: thermal control system liquid heat carrier two-phase thermal control system hydraulic model
Authors:
N.А. Testoyedov - Dr.Sc. (Eng.), Professor, Corresponding Member of RAS, General Director, The Joint-stock Company Academician M.F. Reshetnev «Information Satellite Systems», Zheleznogorsk, Krasnoyarsk region. E-mail: office@iss-reshetnev.ru
E.B. Krivov - Leading Designer, The Joint-stock Company Academician M.F. Reshetnev «Information Satellite Systems», Zheleznogorsk, Krasnoyarsk Region. E-mail: krivov@iss-reshetnev.ru
Abstract:
The article suggests the thermal control system with the fluid loop and two-phase subsystem with deployable radiator for future communications satellites to provide cold-productivity more than 9 kW. The mathematical hydraulic models of liquid circuits and two-phase subsystems. The basis of the thermal control system is fluid loop with two-phase subsystem with deployable radiator. Implementation of the combined the thermal control systems possible, taking into account the accumulated experience of JSC "ISS" when creating the thermal control systems with the circulation of a liquid heat-carrier and the positive results of tests of loop heat pipes with thermal interface with the liquid circulating heat bus.
Pages: 29-33
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