DocumentCode :
116721
Title :
Mathematical modeling of single-phase thermal control system of the spacecraft
Author :
Delcov, A.V. ; Hodenkov, A.A. ; Zhuikov, D.A.
Author_Institution :
Siberian State Aerosp. Univ. named after Academician M.F. Reshetnev, Krasnoyarsk, Russia
fYear :
2014
fDate :
2-4 Oct. 2014
Firstpage :
591
Lastpage :
593
Abstract :
This article discusses the modeling of heat transfer in elementary contour-phase thermal control system. Calculated relations to characterize the circuit are given. Results of calculation are described. Problems and prospects of mathematical modeling of systems of spacecraft thermal control are evaluated.
Keywords :
aerospace control; mathematical analysis; space vehicles; thermal variables control; heat transfer; mathematical modeling; single phase thermal control system; spacecraft thermal control; Fluids; Heat transfer; Mathematical model; Space heating; Temperature; Mathematical modeling; thermal control system;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Actual Problems of Electronics Instrument Engineering (APEIE), 2014 12th International Conference on
Conference_Location :
Novosibirsk
Print_ISBN :
978-1-4799-6019-4
Type :
conf
DOI :
10.1109/APEIE.2014.7040754
Filename :
7040754
Link To Document :
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