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