Use of Solar Panels in the Design of Small CubeSat Spacecraft

The article discusses organization of power supply for small spacecraft of CubeSat type. Various methods of power supply of CubeSat onboard equipment are worked out. The use of solar panels (SP) for power supply of CubeSat is proposed. The developed technology for the production of solar arrays of t...

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Autores principales:	Selivanov Kirill V., Vasiliev Igor A., Yakovenko Arina A.
Formato:	article
Lenguaje:	EN FR
Publicado:	EDP Sciences 2021
Materias:	Engineering (General). Civil engineering (General) TA1-2040
Acceso en línea:	https://doaj.org/article/708d809b9dc6461897eb899a7a3374b7
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id	oai:doaj.org-article:708d809b9dc6461897eb899a7a3374b7
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spelling	oai:doaj.org-article:708d809b9dc6461897eb899a7a3374b72021-11-08T15:20:43ZUse of Solar Panels in the Design of Small CubeSat Spacecraft2261-236X10.1051/matecconf/202134603029https://doaj.org/article/708d809b9dc6461897eb899a7a3374b72021-01-01T00:00:00Zhttps://www.matec-conferences.org/articles/matecconf/pdf/2021/15/matecconf_icmtmte2021_03029.pdfhttps://doaj.org/toc/2261-236XThe article discusses organization of power supply for small spacecraft of CubeSat type. Various methods of power supply of CubeSat onboard equipment are worked out. The use of solar panels (SP) for power supply of CubeSat is proposed. The developed technology for the production of solar arrays of the required size from solar panels has been demonstrated. The organization of incoming control of solar panels to improve reliability and achieve maximum efficiency of produced solar panels is considered. A developed stand for diagnostics of solar cells, which allows detecting latent defects, is presented. The issue of determining power characteristics of the developed solar panels and the necessary optimal load for their maximum efficiency is discussed. The installation of solar panels on the CubeSat aircraft is described. The efficiency of solar panels is tested in space by launching CubeSat on a stratospheric probe. The parameters of the aircraft current supply and current generation by solar panels obtained as a result of the experiment are collected and processed, the results are presented in the article in the form of graphs. On basis of the data obtained, effectiveness of the use of solar panels on small aircraft of the CubeSat type is shown.Selivanov Kirill V.Vasiliev Igor A.Yakovenko Arina A.EDP SciencesarticleEngineering (General). Civil engineering (General)TA1-2040ENFRMATEC Web of Conferences, Vol 346, p 03029 (2021)
institution	DOAJ
collection	DOAJ
language	EN FR
topic	Engineering (General). Civil engineering (General) TA1-2040
spellingShingle	Engineering (General). Civil engineering (General) TA1-2040 Selivanov Kirill V. Vasiliev Igor A. Yakovenko Arina A. Use of Solar Panels in the Design of Small CubeSat Spacecraft
description	The article discusses organization of power supply for small spacecraft of CubeSat type. Various methods of power supply of CubeSat onboard equipment are worked out. The use of solar panels (SP) for power supply of CubeSat is proposed. The developed technology for the production of solar arrays of the required size from solar panels has been demonstrated. The organization of incoming control of solar panels to improve reliability and achieve maximum efficiency of produced solar panels is considered. A developed stand for diagnostics of solar cells, which allows detecting latent defects, is presented. The issue of determining power characteristics of the developed solar panels and the necessary optimal load for their maximum efficiency is discussed. The installation of solar panels on the CubeSat aircraft is described. The efficiency of solar panels is tested in space by launching CubeSat on a stratospheric probe. The parameters of the aircraft current supply and current generation by solar panels obtained as a result of the experiment are collected and processed, the results are presented in the article in the form of graphs. On basis of the data obtained, effectiveness of the use of solar panels on small aircraft of the CubeSat type is shown.
format	article
author	Selivanov Kirill V. Vasiliev Igor A. Yakovenko Arina A.
author_facet	Selivanov Kirill V. Vasiliev Igor A. Yakovenko Arina A.
author_sort	Selivanov Kirill V.
title	Use of Solar Panels in the Design of Small CubeSat Spacecraft
title_short	Use of Solar Panels in the Design of Small CubeSat Spacecraft
title_full	Use of Solar Panels in the Design of Small CubeSat Spacecraft
title_fullStr	Use of Solar Panels in the Design of Small CubeSat Spacecraft
title_full_unstemmed	Use of Solar Panels in the Design of Small CubeSat Spacecraft
title_sort	use of solar panels in the design of small cubesat spacecraft
publisher	EDP Sciences
publishDate	2021
url	https://doaj.org/article/708d809b9dc6461897eb899a7a3374b7
work_keys_str_mv	AT selivanovkirillv useofsolarpanelsinthedesignofsmallcubesatspacecraft AT vasilievigora useofsolarpanelsinthedesignofsmallcubesatspacecraft AT yakovenkoarinaa useofsolarpanelsinthedesignofsmallcubesatspacecraft
_version_	1718441759885754368

Use of Solar Panels in the Design of Small CubeSat Spacecraft

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