Teplofizika vysokikh temperatur
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Teplofizika vysokikh temperatur, 2017, Volume 55, Issue 1, Pages 108–114
DOI: https://doi.org/10.7868/S0040364417010094
(Mi tvt10077)
 

This article is cited in 13 scientific papers (total in 13 papers)

Heat and Mass Transfer and Physical Gasdynamics

Optimal way for choosing parameters of spacecraft’s screen-vacuum heat insulation

V. F. Formalev, S. A. Kolesnik, I. A. Selin, E. L. Kuznetsova

Moscow Aviation Institute (National Research University)
References:
Abstract: The heat transfer in multiple plate sandwiches of spacecraft’s screen-vacuum heat insulation is simulated for determining the characteristics of heat shielding against long-term solar heat flux. To choose optimal characteristics of heat shielding, it is necessary to determine precisely the number of plates and their peculiarities. The new, absolutely stable method for solving numerically heat transfer problems is presented. We obtain results showing that the screen-vacuum insulation is characterized by low heating-up inertance that is unacceptable. To remove this effect, the inertial heat shielding is used on the internal surface of the heat shielding and its state is examined.
Received: 07.12.2015
Accepted: 22.12.2015
English version:
High Temperature, 2017, Volume 55, Issue 1, Pages 101–106
DOI: https://doi.org/10.1134/S0018151X17010096
Bibliographic databases:
Document Type: Article
UDC: 536.21
Language: Russian
Citation: V. F. Formalev, S. A. Kolesnik, I. A. Selin, E. L. Kuznetsova, “Optimal way for choosing parameters of spacecraft’s screen-vacuum heat insulation”, TVT, 55:1 (2017), 108–114; High Temperature, 55:1 (2017), 101–106
Citation in format AMSBIB
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\pages 108--114
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  • https://www.mathnet.ru/eng/tvt/v55/i1/p108
  • This publication is cited in the following 13 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    Teplofizika vysokikh temperatur Teplofizika vysokikh temperatur
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