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| Título: | Thermal Analysis of the Solar Orbiter PHI Electronics Unit |
Autor: | Torralbo Gimeno, Ignacio; Pérez Grande, Isabel; Gasent-Blesa, José Luis; Piqueras J.; Sanchis Kilders, Esteban; Rodriguez P.; López Jiménez, A. C. CSIC ORCID | Palabras clave: | Integrated circuit thermal modeling Scientific instrument electronics Space instrumentation Space thermal control Thermal management of space electronics Thermal modeling Testing |
Fecha de publicación: | 2020 | Editor: | Institute of Electrical and Electronics Engineers | Citación: | IEEE Transactions on Aerospace and Electronic Systems 56(1): 186-195 (2020) | Resumen: | 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. | Descripción: | “© 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.” | Versión del editor: | 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 |
| Aparece en las colecciones: | (IAA) Artículos |
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| IAA_2020_TAES2911734.pdf | 4,68 MB | Adobe PDF |  Visualizar/Abrir |
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