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dc.contributor.authorGarcia Luis, Uxia 
dc.contributor.authorNavarro Medina, Fermín 
dc.contributor.authorUlloa Sande, Carlos 
dc.contributor.authorGomez San Juan, Alejandro Manuel 
dc.contributor.authorRey González, Guillermo David 
dc.contributor.authorPires, Ana
dc.contributor.authorMaia, Margarida
dc.contributor.authorRocha, Mariana
dc.contributor.authorAguado Agelet, Fernando Antonio 
dc.date.accessioned2024-03-21T09:42:35Z
dc.date.issued2023-11-18
dc.identifier.citationCEAS Space Journal, 2023(18-11): 18-11 (2023)spa
dc.identifier.issn18682502
dc.identifier.issn18682510
dc.identifier.urihttp://hdl.handle.net/11093/6471
dc.description.abstractWireless energy transfer (WET) devices using arrays of hybrid photo-thermoelectric plasmonic (HPTP) generators are under investigation to be a potential power source choice for CubeSats. This power generation system is based on the conversion of photon energy into electric energy via thermal gradients employing a large-range pulsed laser as source. During the study of the devices’ integration on board a 3U CubeSat, the thermal subsystem was identified as the most critical, and thus its study has a major relevance for the demonstration of the technology herein proposed. The methodology employed to characterize the HPTP generators within the CubeSat thermal model is shown in this paper. From here, we cover the influence of the most significant model parameters under a given operational case, as well as a comparison on the performance of different thermoelectric devices configurations. Overall, the results show a maximization of the power obtained with the circular cells configuration and a very small variation in the temperature field with changes in the most significant parameters in the ranges dictated by the European Cooperation for Space Standardization (ECSS) that enables high reliability on the results that could be obtained from the model, despite the uncertainty inherent in a sensitivity study at the early stages of the project development.en
dc.description.sponsorshipFundação para a Ciência e a Tecnologiaspa
dc.language.isoengspa
dc.publisherCEAS Space Journalspa
dc.rightsCopyright © 2023, The Author(s), under exclusive licence to Council of European Aerospace Societies
dc.titleModelling and preliminary thermal study of a fed-by-laser thermoelectric generator system on board of a 3U CubeSaten
dc.typearticlespa
dc.rights.accessRightsclosedAccessspa
dc.relation.projectIDinfo:eu-repo/grantAgreement/EC/H2020/863307spa
dc.identifier.doi10.1007/s12567-023-00528-6
dc.identifier.editorhttps://link.springer.com/10.1007/s12567-023-00528-6spa
dc.publisher.departamentoEnxeñaría mecánica, máquinas e motores térmicos e fluídosspa
dc.publisher.departamentoTeoría do sinal e comunicaciónsspa
dc.publisher.grupoinvestigacionGrupo de Tecnoloxías Aeroespaciaisspa
dc.subject.unesco3324 Tecnología del Espaciospa
dc.date.embargoEndDateindefinidospa
dc.date.updated2024-03-20T19:12:48Z
dc.computerCitationpub_title=CEAS Space Journal|volume=2023|journal_number=18-11|start_pag=18-11|end_pag=spa


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