Numerical analysis of thermal radiation of spacecraft on orbit based on SINDA/FLUINT

Numerical analysis of thermal radiation of spacecraft on orbit based on SINDA/FLUINT

Thermal stability is an important indicator to measure the reliability of aerospace equipment, and the space thermal environment is complex, and the commonly used thermal analysis software for ground equipment can no longer meet the needs. For this reason, based on the thermal design analysis softwa...

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Main Author: Shi Yi
Format: Article
Language:English
Published: EDP Sciences 2021-01-01
Series:E3S Web of Conferences
Online Access:https://www.e3s-conferences.org/articles/e3sconf/pdf/2021/37/e3sconf_icemee2021_02024.pdf
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spelling doaj-53af1e6598e941a2a03222d5484f0eda2021-05-28T14:41:32ZengEDP SciencesE3S Web of Conferences2267-12422021-01-012610202410.1051/e3sconf/202126102024e3sconf_icemee2021_02024Numerical analysis of thermal radiation of spacecraft on orbit based on SINDA/FLUINTShi Yi0Institute of Thermal Science Technology, Shandong UniversityThermal stability is an important indicator to measure the reliability of aerospace equipment, and the space thermal environment is complex, and the commonly used thermal analysis software for ground equipment can no longer meet the needs. For this reason, based on the thermal design analysis software SINDA/FLUINT, taking a spacecraft as the research object, the thermal balance equation is first established. Then, use the thermal desktop software to establish a numerical model, and use the SINDA/FLUINT software to solve the heat transfer process. Finally, the thermal desktop is used to post-process the calculation results and analyse the thermal radiation of the spacecraft.https://www.e3s-conferences.org/articles/e3sconf/pdf/2021/37/e3sconf_icemee2021_02024.pdf
collection DOAJ
language English
format Article
sources DOAJ
author Shi Yi
spellingShingle Shi Yi
Numerical analysis of thermal radiation of spacecraft on orbit based on SINDA/FLUINT
E3S Web of Conferences
author_facet Shi Yi
author_sort Shi Yi
title Numerical analysis of thermal radiation of spacecraft on orbit based on SINDA/FLUINT
title_short Numerical analysis of thermal radiation of spacecraft on orbit based on SINDA/FLUINT
title_full Numerical analysis of thermal radiation of spacecraft on orbit based on SINDA/FLUINT
title_fullStr Numerical analysis of thermal radiation of spacecraft on orbit based on SINDA/FLUINT
title_full_unstemmed Numerical analysis of thermal radiation of spacecraft on orbit based on SINDA/FLUINT
title_sort numerical analysis of thermal radiation of spacecraft on orbit based on sinda/fluint
publisher EDP Sciences
series E3S Web of Conferences
issn 2267-1242
publishDate 2021-01-01
description Thermal stability is an important indicator to measure the reliability of aerospace equipment, and the space thermal environment is complex, and the commonly used thermal analysis software for ground equipment can no longer meet the needs. For this reason, based on the thermal design analysis software SINDA/FLUINT, taking a spacecraft as the research object, the thermal balance equation is first established. Then, use the thermal desktop software to establish a numerical model, and use the SINDA/FLUINT software to solve the heat transfer process. Finally, the thermal desktop is used to post-process the calculation results and analyse the thermal radiation of the spacecraft.
url https://www.e3s-conferences.org/articles/e3sconf/pdf/2021/37/e3sconf_icemee2021_02024.pdf
work_keys_str_mv AT shiyi numericalanalysisofthermalradiationofspacecraftonorbitbasedonsindafluint
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