The effect of the PCB solder mask type of the hull outer surface of the CubeSat 3U on its thermal regime

V. N. Gorev; A. A. Kozlov; V. Yu Prokopyev; Yu M. Prokopyev; A. S. Stuf; A. A. Sidorchuk

doi:10.1088/1757-899X/734/1/012027

The effect of the PCB solder mask type of the hull outer surface of the CubeSat 3U on its thermal regime

V. N. Gorev, A. A. Kozlov, V. Yu Prokopyev, Yu M. Prokopyev, A. S. Stuf, A. A. Sidorchuk

Результат исследования: Научные публикации в периодических изданиях › статья по материалам конференции › рецензирование

1 Цитирования (Scopus)

Аннотация

Rather simple methods to measure the absorbed solar radiation coefficients and IR radiation, as well as optical coefficients measured by these methods for the construction materials of microsatellites and PCB coated with different solder masks are presented. The calculating results of the satellite's thermal conditions for different PCB solder masks at the satellite outer surface are given. The thermal model is implemented on the orbital motion and insolation calculating algorithm basis, which developed in Matlab Simulink. A CubeSat 3U type satellite with foldable solar panels is considered as an example.

Язык оригинала	английский
Номер статьи	012027
Журнал	IOP Conference Series: Materials Science and Engineering
Том	734
Номер выпуска	1
DOI	https://doi.org/10.1088/1757-899X/734/1/012027
Состояние	Опубликовано - 29 янв 2020
Событие	2nd International Scientific Conference on Advanced Technologies in Aerospace, Mechanical and Automation Engineering, MIST: Aerospace 2019 - Krasnoyarsk, Российская Федерация Продолжительность: 18 ноя 2019 → 21 ноя 2019

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10.1088/1757-899X/734/1/012027

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title = "The effect of the PCB solder mask type of the hull outer surface of the CubeSat 3U on its thermal regime",

abstract = "Rather simple methods to measure the absorbed solar radiation coefficients and IR radiation, as well as optical coefficients measured by these methods for the construction materials of microsatellites and PCB coated with different solder masks are presented. The calculating results of the satellite's thermal conditions for different PCB solder masks at the satellite outer surface are given. The thermal model is implemented on the orbital motion and insolation calculating algorithm basis, which developed in Matlab Simulink. A CubeSat 3U type satellite with foldable solar panels is considered as an example.",

author = "Gorev, {V. N.} and Kozlov, {A. A.} and Prokopyev, {V. Yu} and Prokopyev, {Yu M.} and Stuf, {A. S.} and Sidorchuk, {A. A.}",

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The effect of the PCB solder mask type of the hull outer surface of the CubeSat 3U on its thermal regime. / Gorev, V. N.; Kozlov, A. A.; Prokopyev, V. Yu ; Prokopyev, Yu M.; Stuf, A. S.; Sidorchuk, A. A.

В: IOP Conference Series: Materials Science and Engineering, Том 734, № 1, 012027, 29.01.2020.

Результат исследования: Научные публикации в периодических изданиях › статья по материалам конференции › рецензирование

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AU - Gorev, V. N.

AU - Kozlov, A. A.

AU - Prokopyev, V. Yu

AU - Prokopyev, Yu M.

AU - Stuf, A. S.

AU - Sidorchuk, A. A.

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N2 - Rather simple methods to measure the absorbed solar radiation coefficients and IR radiation, as well as optical coefficients measured by these methods for the construction materials of microsatellites and PCB coated with different solder masks are presented. The calculating results of the satellite's thermal conditions for different PCB solder masks at the satellite outer surface are given. The thermal model is implemented on the orbital motion and insolation calculating algorithm basis, which developed in Matlab Simulink. A CubeSat 3U type satellite with foldable solar panels is considered as an example.

AB - Rather simple methods to measure the absorbed solar radiation coefficients and IR radiation, as well as optical coefficients measured by these methods for the construction materials of microsatellites and PCB coated with different solder masks are presented. The calculating results of the satellite's thermal conditions for different PCB solder masks at the satellite outer surface are given. The thermal model is implemented on the orbital motion and insolation calculating algorithm basis, which developed in Matlab Simulink. A CubeSat 3U type satellite with foldable solar panels is considered as an example.

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