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Space Research
Reference:

A method for estimating the thermal regime of solar panels when performing angular turns of the Earth observation satellite

Steganov Gennadii Borisovich

PhD in Technical Science

Docent, the department of Avionics and Aircraft Electrical Systems, A. F. Mozhaysky's Military-Space Academy

197198, Russia, Leningradskaya oblast', g. Saint Petersburg, ul. Zhdanovskaya, 13

vka_22kaf-maleninen@rambler.ru
Kargu Dmitrii Leonidovich

PhD in Technical Science

Docent, the department of Avionics and Aircraft Electrical Systems, A. F. Mozhaysky's Military-Space Academy

197198, Russia, Leningradskaya oblast', g. Saint Petersburg, ul. Zhdanovskaya, 13

vka_22kaf-maleninen@rambler.ru
Malenin Evgenii Nikolaevich

PhD in Technical Science

Senior Educator, the department of Avionics and Aircraft Electrical Systems, A. F. Mozhaysky's Military-Space Academy

197198, Russia, Leningradskaya oblast', g. Saint Petersburg, ul. Zhdanovskaya, 13

vka_22kaf-maleninen@rambler.ru
Yanguzov Andrei Valerievich

Senior Engineer, Militaty Unit No.13973

197198, Russia, Leningradskaya oblast', g. Saint Petersburg, ul. Zhdanovskaya, 13

izlow427@mail.ru

DOI:

10.7256/2453-8817.2019.2.31434

Review date:

20-11-2019


Publish date:

13-02-2020


Abstract.

The results of modeling the thermal operation of solar panels (PSB) of the Earth observation satellite (EOS) when moving in a circular orbit are presented. Modeling of the thermal regime is carried out for two groups of photovoltaic converters (FEP). FEPs are conventionally divided into groups, depending on the strength of the influence of different heat fluxes characteristic of the movement of the satellite in a circular orbit. Analytical expressions for the heat balance equation of the PSBs and the results of numerical calculations at the end of the active life (SAC) are given. In this work, methods of deduction, induction, analysis, modeling, formalization, experiment, as well as statistical method, system and structural-functional method were used. The presented model for calculating the temperature of the solar panel of the Earth observation satellite is a set of mathematical expressions that allow calculating temperature of any FEP within a particular solar panel and make adjustments to the plan of exploitation.

Keywords: the ratio of reradiation of solar cells, heat flow, photoelectric converter, earth remote sensing spacecraft, heat balance, solar panel, thermal model, output power, heat-exchange, the temperature of the solar cells
This article written in Russian. You can find full text of article in Russian here .

References
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Malozemov V. V. Teplovoi rezhim kosmicheskikh apparatov. M.: Mashinostroenie, 1980. 232 s.
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Shubin D. A., Kargu D. L., Astakhov N. N., Gorbulin V. I., Steganov G. B. Matematicheskaya modelirovanie dinamiki temperatury solnechnykh batarei v razlichnykh usloviyakh orbital'nogo poleta kosmicheskogo apparata // Vestnik Moskovskogo gosudarstvennogo tekhnicheskogo universiteta imeni N. E. Baumana. Seriya: Mashinostroenie. 2016. Vyp. 6 (111). S. 4-21.
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Tsaplin S.V., Bolychev S.A., Romanov A.E. Teploobmen v kosmose. Samara: Samarskii universitet, 2013. 56 s.
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