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Thermal Analysis of the Solar Orbiter PHI Electronics Unit

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Thermal Analysis of the Solar Orbiter PHI Electronics Unit

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dc.contributor.author	Torralbo, Ignacio
dc.contributor.author	Pérez Grande, Isabel
dc.contributor.author	Gasent Blesa, José Luis
dc.contributor.author	Piqueras, Javier
dc.contributor.author	Sanchis Kilders, Esteban
dc.contributor.author	Rodriguez, Pedro
dc.contributor.author	López, Antonio
dc.date.accessioned	2023-11-23T08:27:58Z
dc.date.available	2023-11-23T08:27:58Z
dc.date.issued	2020
dc.identifier.uri	https://hdl.handle.net/10550/91347
dc.description.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.
dc.language.iso	eng
dc.relation.ispartof	IEEE Transactions on Aerospace and Electronic Systems, 2020, vol. 56, num. 1, p. 186-195
dc.source	I. Torralbo et al., "Thermal Analysis of the Solar Orbiter PHI Electronics Unit," in IEEE Transactions on Aerospace and Electronic Systems, vol. 56, no. 1, pp. 186-195, Feb. 2020, doi: 10.1109/TAES.2019.2911734.
dc.subject	electrònica
dc.subject	física
dc.title	Thermal Analysis of the Solar Orbiter PHI Electronics Unit
dc.type	journal article
dc.date.updated	2023-11-23T08:27:58Z
dc.identifier.doi	10.1109/TAES.2019.2911734
dc.identifier.idgrec	142234
dc.rights.accessRights	open access