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Study: Development of a numerical model of the thermal behaviour of a CubeSat

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hdl:2117/188654

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Gort Mas, Marc
Tutor / directorSoria Guerrero, ManelMés informacióMés informacióMés informació
Document typeMaster thesis
Date2018-06-20
Rights accessRestricted access - author's decision
All rights reserved. This work is protected by the corresponding intellectual and industrial property rights. Without prejudice to any existing legal exemptions, reproduction, distribution, public communication or transformation of this work are prohibited without permission of the copyright holder
Abstract
The thermal analysis of CubeSats is an essential part of the design of this type ofsatellite, but it is often difficult to achieve due to the need for expensive commer-cial software and the complexity of thermal modelling. In this study, a softwarespecialised on the thermal analysis of CubeSats is developed. This software allowsto easily define a CubeSat model and boundary and initial conditions, and thensimulates its internal thermal behaviour by taking into account thermal conduc-tion, contact conductance, and radiation. The results for a representative CubeSatmodel have been compared to those obtained with Thermal Desktop for an equiv-alent model, and the maximum temperature differences between both programshave been found to stay around 2 to 5◦C.
SubjectsArtificial satellites, Thermodynamics--Mathematical models, Satèl·lits artificials, Termodinàmica -- Models matemàtics
DegreeMÀSTER UNIVERSITARI EN ENGINYERIA AERONÀUTICA (Pla 2014)
URIhttp://hdl.handle.net/2117/188654
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  • Màsters oficials - Màster universitari en Enginyeria Aeronàutica [244]
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REPORT_575.pdfBlocked1,846MbPDFRestricted access
BUDGET_584.pdfBlocked83,21KbPDFRestricted access
Assessment.pdfBlocked343,7KbPDFRestricted access

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