A university small satellite thermal control modeling and analysis in the post-mission phase

This work includes the thermal control analysis of a small spacecraft in the post-mission phase. The satellite internal component distribution has been modified to fulfill all thermal requirements when using a passive thermal control system. In the post-mission phase, the satellite will be used by t...

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Autores principales:	Elhefnawy Ahmed, Elmaihy Ali, Elweteedy Ahmed
Formato:	article
Lenguaje:	EN
Publicado:	University of Belgrade - Faculty of Mechanical Engineering, Belgrade 2021
Materias:	aerospace engineering satellite thermal control modeling Engineering (General). Civil engineering (General) TA1-2040 Mechanics of engineering. Applied mechanics TA349-359
Acceso en línea:	https://doaj.org/article/0995ee638c3c4d2baaaf49fd94eea919
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spelling	oai:doaj.org-article:0995ee638c3c4d2baaaf49fd94eea9192021-12-05T21:01:51ZA university small satellite thermal control modeling and analysis in the post-mission phase1451-20922406-128X10.5937/fme2104014Ehttps://doaj.org/article/0995ee638c3c4d2baaaf49fd94eea9192021-01-01T00:00:00Zhttps://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2021/1451-20922104014E.pdfhttps://doaj.org/toc/1451-2092https://doaj.org/toc/2406-128XThis work includes the thermal control analysis of a small spacecraft in the post-mission phase. The satellite internal component distribution has been modified to fulfill all thermal requirements when using a passive thermal control system. In the post-mission phase, the satellite will be used by the radio Amateur Satellite Corporation (AMSAT) community as a transponder, fully using the AMSAT payload that will maintain active and shall last at least 2 years. Thermal Desktop software is introduced for the mentioned spacecraft. The final analysis predictions show that the passive thermal control system maintains all satellite element's temperatures within their temperature limits. The temperature variation of +X solar panel is 75 °C which is less than experienced by +Z and -Z panels, which are 100 °C. The temperature change on equipment agrees with their panels. Compared with a specialized thermal analysis, software package (ESATAN-TMSs) verified the integrity of the results.Elhefnawy AhmedElmaihy AliElweteedy AhmedUniversity of Belgrade - Faculty of Mechanical Engineering, Belgradearticleaerospace engineeringsatellite thermal controlmodelingEngineering (General). Civil engineering (General)TA1-2040Mechanics of engineering. Applied mechanicsTA349-359ENFME Transactions, Vol 49, Iss 4, Pp 1014-1024 (2021)
institution	DOAJ
collection	DOAJ
language	EN
topic	aerospace engineering satellite thermal control modeling Engineering (General). Civil engineering (General) TA1-2040 Mechanics of engineering. Applied mechanics TA349-359
spellingShingle	aerospace engineering satellite thermal control modeling Engineering (General). Civil engineering (General) TA1-2040 Mechanics of engineering. Applied mechanics TA349-359 Elhefnawy Ahmed Elmaihy Ali Elweteedy Ahmed A university small satellite thermal control modeling and analysis in the post-mission phase
description	This work includes the thermal control analysis of a small spacecraft in the post-mission phase. The satellite internal component distribution has been modified to fulfill all thermal requirements when using a passive thermal control system. In the post-mission phase, the satellite will be used by the radio Amateur Satellite Corporation (AMSAT) community as a transponder, fully using the AMSAT payload that will maintain active and shall last at least 2 years. Thermal Desktop software is introduced for the mentioned spacecraft. The final analysis predictions show that the passive thermal control system maintains all satellite element's temperatures within their temperature limits. The temperature variation of +X solar panel is 75 °C which is less than experienced by +Z and -Z panels, which are 100 °C. The temperature change on equipment agrees with their panels. Compared with a specialized thermal analysis, software package (ESATAN-TMSs) verified the integrity of the results.
format	article
author	Elhefnawy Ahmed Elmaihy Ali Elweteedy Ahmed
author_facet	Elhefnawy Ahmed Elmaihy Ali Elweteedy Ahmed
author_sort	Elhefnawy Ahmed
title	A university small satellite thermal control modeling and analysis in the post-mission phase
title_short	A university small satellite thermal control modeling and analysis in the post-mission phase
title_full	A university small satellite thermal control modeling and analysis in the post-mission phase
title_fullStr	A university small satellite thermal control modeling and analysis in the post-mission phase
title_full_unstemmed	A university small satellite thermal control modeling and analysis in the post-mission phase
title_sort	university small satellite thermal control modeling and analysis in the post-mission phase
publisher	University of Belgrade - Faculty of Mechanical Engineering, Belgrade
publishDate	2021
url	https://doaj.org/article/0995ee638c3c4d2baaaf49fd94eea919
work_keys_str_mv	AT elhefnawyahmed auniversitysmallsatellitethermalcontrolmodelingandanalysisinthepostmissionphase AT elmaihyali auniversitysmallsatellitethermalcontrolmodelingandanalysisinthepostmissionphase AT elweteedyahmed auniversitysmallsatellitethermalcontrolmodelingandanalysisinthepostmissionphase AT elhefnawyahmed universitysmallsatellitethermalcontrolmodelingandanalysisinthepostmissionphase AT elmaihyali universitysmallsatellitethermalcontrolmodelingandanalysisinthepostmissionphase AT elweteedyahmed universitysmallsatellitethermalcontrolmodelingandanalysisinthepostmissionphase
_version_	1718370984619147264

A university small satellite thermal control modeling and analysis in the post-mission phase

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