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Campo DC | Valor | Idioma |
---|---|---|
dc.rights.license | Copyright © 2018, IEEE | es |
dc.contributor.author | Muñoz Hernández, Alfonso | es |
dc.contributor.author | Jiménez Lorenzo, María | es |
dc.contributor.author | Gala Escolar, José | es |
dc.contributor.author | López Sanz, Daniel | es |
dc.contributor.author | Arnau Trillol, Alejandro | es |
dc.contributor.author | Añón Cancela, M. | es |
dc.date.accessioned | 2023-01-12T12:17:10Z | - |
dc.date.available | 2023-01-12T12:17:10Z | - |
dc.date.issued | 2018-10-08 | - |
dc.identifier.citation | Proceedings of the International Symposium on Electromagnetic Compatibility- EU 2018 | es |
dc.identifier.isbn | 9781467396981 | - |
dc.identifier.issn | 2325-0356 | - |
dc.identifier.other | https://ieeexplore.ieee.org/document/8485137 | es |
dc.identifier.uri | http://hdl.handle.net/20.500.12666/828 | - |
dc.description.abstract | The new scientific European Space Agency (ESA) missions are demanding new restrictions for Electromagnetic compatibility (EMC) coming from the scientists. The observation of the deep space, our closer planets and stars requires the measurement of very low Electric and Magnetic fields that imposes important challenges of EMC compatibility for all the on-board equipment of the satellite. This paper presents these new requirements for emission (E-field and H-field) and magnetic fields for two of the last ESA mission; Solar Orbiter and Juice and compare them with the standards requirement coming from the ESA standards. These challenges will appear in two of the development phases: design phase and verification phases. These new requirements shall be taking into account in the design but also during the verification and testing. The measurements required for the verification of these requirements are also an important challenge. This paper shown the test challenge during the verification. | es |
dc.description.sponsorship | Thanks to all the SENER Solar Orbiter & Juice design and testing team that works together to analyses and meet the requirements in these missions. This work was funded in part by the Spanish Ministry of Economy, Industry and Competitiveness (MEIC) within the project UAVE3 (TEC2016-79214-C3-1-R). | es |
dc.language.iso | eng | es |
dc.publisher | Institute of Electrical and Electronics Engineers | es |
dc.relation | info:eu-repo/grantAgreement/AEI/Plan Estatal de Investigación Científica y Técnica y de Innovación 2013-2016/TEC2016-79214-C3-1-R/ES/EVALUACION NUMERICA Y EXPERIMENTAL DE EFECTOS ELECTROMAGNETICOS AMBIENTALES EN AVIONES NO TRIPULADOS/ | es |
dc.subject | Electric field | es |
dc.subject | Radiated emission | es |
dc.subject | EMC | es |
dc.subject | Test verification | es |
dc.title | EMC Challenges for ESA Scientific Missions | es |
dc.type | info:eu-repo/semantics/conferenceObject | es |
dc.identifier.e-issn | 2325-0364 | - |
dc.contributor.funder | Agencia Estatal de Investigación (AEI) | es |
dc.description.peerreviewed | Preprint | es |
dc.type.hasVersion | info:eu-repo/semantics/publishedVersion | es |
dc.rights.accessRights | info:eu-repo/semantics/restrictedAccess | es |
dc.type.coar | http://purl.org/coar/resource_type/c_18cf | es |
Aparece en las colecciones: | (Espacio) Comunicaciones de Congresos |
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