Email this article Analysis of Efficiency of Systems for Control of the Thermal Regime of Spacecraft
- Authors: Delkov A.V.1, Kishkin A.A.1, Lavrov N.A.2, Tanasienko F.V.3
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Affiliations:
- Siberian State Aerospace University
- Bauman Moscow State Technical University
- Reshetnev Information Satellite Systems
- Issue: Vol 51, No 9-10 (2016)
- Pages: 714-719
- Section: Article
- URL: https://journal-vniispk.ru/0009-2355/article/view/234229
- DOI: https://doi.org/10.1007/s10556-016-0110-z
- ID: 234229
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Abstract
Problems and the outlook for the development of effective systems of controlling the thermal regimes of spacecraft are considered. The process of creating and using the apparatus of mathematical modeling for the purpose of comparing the energy characteristics of different systems is described. The characteristics of forward and reverse working cycles of two-phase closed systems that control the thermal regimes are compared.
About the authors
A. V. Delkov
Siberian State Aerospace University
Author for correspondence.
Email: spsp99@mail.ru
Russian Federation, Krasnoyarsk
A. A. Kishkin
Siberian State Aerospace University
Email: lavrov@power.bmstu.ru
Russian Federation, Krasnoyarsk
N. A. Lavrov
Bauman Moscow State Technical University
Author for correspondence.
Email: lavrov@power.bmstu.ru
Russian Federation, Moscow
F. V. Tanasienko
Reshetnev Information Satellite Systems
Email: lavrov@power.bmstu.ru
Russian Federation, Zheznogorsk
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