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Please use this identifier to cite or link to this item: https://dspace.iiti.ac.in/handle/123456789/13772
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dc.contributor.authorSahu, Kundanen_US
dc.contributor.authorShekhar, Kumar Sheshanken_US
dc.contributor.authorDatta, Abhirupen_US
dc.date.accessioned2024-06-28T11:38:16Z-
dc.date.available2024-06-28T11:38:16Z-
dc.date.issued2023-
dc.identifier.citationSahu, K., Tej, B. R. P., Shekhar, K. S., & Datta, A. (2023). Structural and Thermal Analysis of a Modular 1U CubeSat for RFI Survey on LEO orbit. 2023 8th International Conference on Computers and Devices for Communication, CODEC 2023. Scopus. https://doi.org/10.1109/CODEC60112.2023.10466039en_US
dc.identifier.isbn979-8350317176-
dc.identifier.otherEID(2-s2.0-85190068116)-
dc.identifier.urihttps://doi.org/10.1109/CODEC60112.2023.10466039-
dc.identifier.urihttps://dspace.iiti.ac.in/handle/123456789/13772-
dc.description.abstractIn today's space exploration, CubeSats are the preferred choice due to their functionality, cost, and time efficiency. The harsh environment of space exposes them to extreme conditions. In this paper, we analyze the CubeSat's structure and thermal properties and develop a comprehensive model to predict its behavior. In this study, two CubeSat designs are compared showing the importance of load distribution. © 2023 IEEE.en_US
dc.language.isoenen_US
dc.publisherInstitute of Electrical and Electronics Engineers Inc.en_US
dc.source2023 8th International Conference on Computers and Devices for Communication, CODEC 2023en_US
dc.subjectCubeSaten_US
dc.subjectstructural analysisen_US
dc.subjectthermal analysisen_US
dc.titleStructural and Thermal Analysis of a Modular 1U CubeSat for RFI Survey on LEO orbiten_US
dc.typeConference Paperen_US
Appears in Collections:Department of Astronomy, Astrophysics and Space Engineering

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