Analysis of Efficiency of Systems for Control of the Thermal Regime of Spacecraft

A. V. Delkov; A. A. Kishkin; N. A. Lavrov; F. V. Tanasienko

doi:10.1007/s10556-016-0110-z

Analysis of Efficiency of Systems for Control of the Thermal Regime of Spacecraft

作者: Delkov A.V.¹, Kishkin A.A.¹, Lavrov N.A.², Tanasienko F.V.³
隶属关系:
1. Siberian State Aerospace University
2. Bauman Moscow State Technical University
3. Reshetnev Information Satellite Systems
期: 卷 51, 编号 9-10 (2016)
页面: 714-719
栏目: 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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详细

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.