Standard

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 et al.

In: IOP Conference Series: Materials Science and Engineering, Vol. 734, No. 1, 012027, 29.01.2020.

Research output: Contribution to journal › Conference article › peer-review

Harvard

Gorev, VN, Kozlov, AA, Prokopyev, VY, Prokopyev, YM, Stuf, AS & Sidorchuk, AA 2020, 'The effect of the PCB solder mask type of the hull outer surface of the CubeSat 3U on its thermal regime', IOP Conference Series: Materials Science and Engineering, vol. 734, no. 1, 012027. https://doi.org/10.1088/1757-899X/734/1/012027

APA

Gorev, V. N., Kozlov, A. A., Prokopyev, V. Y., Prokopyev, Y. M., Stuf, A. S., & Sidorchuk, A. A. (2020). The effect of the PCB solder mask type of the hull outer surface of the CubeSat 3U on its thermal regime. IOP Conference Series: Materials Science and Engineering, 734(1), [012027]. https://doi.org/10.1088/1757-899X/734/1/012027

Vancouver

Gorev VN, Kozlov AA, Prokopyev VY, Prokopyev YM, Stuf AS, Sidorchuk AA. The effect of the PCB solder mask type of the hull outer surface of the CubeSat 3U on its thermal regime. IOP Conference Series: Materials Science and Engineering. 2020 Jan 29;734(1):012027. doi: 10.1088/1757-899X/734/1/012027

Author

Gorev, V. N. ; Kozlov, A. A. ; Prokopyev, V. Yu et al. / The effect of the PCB solder mask type of the hull outer surface of the CubeSat 3U on its thermal regime. In: IOP Conference Series: Materials Science and Engineering. 2020 ; Vol. 734, No. 1.

BibTeX

@article{d4023895e1204f81ad2b6ae6263020ff,
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.}",
year = "2020",
month = jan,
day = "29",
doi = "10.1088/1757-899X/734/1/012027",
language = "English",
volume = "734",
journal = "IOP Conference Series: Materials Science and Engineering",
issn = "1757-8981",
publisher = "IOP Publishing Ltd.",
number = "1",
note = "2nd International Scientific Conference on Advanced Technologies in Aerospace, Mechanical and Automation Engineering, MIST: Aerospace 2019 ; Conference date: 18-11-2019 Through 21-11-2019",

}

RIS

TY - JOUR

T1 - The effect of the PCB solder mask type of the hull outer surface of the CubeSat 3U on its thermal regime

AU - Gorev, V. N.

AU - Kozlov, A. A.

AU - Prokopyev, V. Yu

AU - Prokopyev, Yu M.

AU - Stuf, A. S.

AU - Sidorchuk, A. A.

PY - 2020/1/29

Y1 - 2020/1/29

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.

UR - http://www.scopus.com/inward/record.url?scp=85079608725&partnerID=8YFLogxK

U2 - 10.1088/1757-899X/734/1/012027

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

M3 - Conference article

AN - SCOPUS:85079608725

VL - 734

JO - IOP Conference Series: Materials Science and Engineering

JF - IOP Conference Series: Materials Science and Engineering

SN - 1757-8981

IS - 1

M1 - 012027

T2 - 2nd International Scientific Conference on Advanced Technologies in Aerospace, Mechanical and Automation Engineering, MIST: Aerospace 2019

Y2 - 18 November 2019 through 21 November 2019

ER -

ID: 23593114