Thermal Analysis of the Solar Orbiter PHI Electronics Unit

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Title:	Thermal Analysis of the Solar Orbiter PHI Electronics Unit
Authors:	Torralbo I.; Perez-Grande I.; Gasent-Blesa J. L.; Piqueras J.; Sanchis-Kilders E.; Rodriguez P.; López Jiménez, A. C.
Keywords:	Integrated circuit thermal modeling Scientific instrument electronics Space instrumentation Space thermal control Thermal management of space electronics Thermal modeling Testing
Issue Date:	2020
Publisher:	Institute of Electrical and Electronics Engineers
Citation:	IEEE Transactions on Aerospace and Electronic Systems 56(1): 186-195 (2020)
Abstract:	This paper presents the thermal design of the electronics unit of the instrument Polarimetric Helioseismic Imager, onboard the European Space Agency mission Solar Orbiter. The thermal design procedure, along with the problems encountered during this design phase, and the solutions found to fix them are described, proving in this way the thermal feasibility and robustness of the unit. Its final thermal behaviour, obtained from thermal analyses correlated with data from thermal tests performed in a vacuum environment, is presented. © 1965-2011 IEEE.
Description:	“© 2020 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.”
Publisher version (URL):	http://dx.doi.org/10.1109/TAES.2019.2911734
URI:	http://hdl.handle.net/10261/212978
DOI:	10.1109/TAES.2019.2911734
ISSN:	0018-9251
Appears in Collections:	(IAA) Artículos

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