Publicación:
Design of a planetary protection cover for EMC testing of a spacial magnetic sensor

dc.contributor.authorFernández Romero, S.es
dc.contributor.authorParrondo, M. C.es
dc.contributor.authorDíaz Michelena, M.es
dc.contributor.authorMuñóz Rebate, I.es
dc.contributor.authorLeón Calero, Marinaes
dc.contributor.authorMartín Iglesias, S.es
dc.contributor.authorPlaza Gallardo, B.es
dc.contributor.authorEscot Bocanegra, D.es
dc.contributor.authorPoyatos Martínez, D.es
dc.contributor.authorJiménez Lorenzo, Maríaes
dc.contributor.authorLópez Sanz, Danieles
dc.contributor.funderMinisterio de Economía y Competitividad (MINECO)es
dc.contributor.funderAgencia Estatal de Investigación (AEI)es
dc.date.accessioned2022-09-20T11:52:32Z
dc.date.available2022-09-20T11:52:32Z
dc.date.issued2019-10-17
dc.description.abstractThis paper explains the research process carried out for the development and manufacture of the planetary protection cover for carrying out the electromagnetic compatibility (EMC) tests of the an-isotropic magneto-resistance (AMR) sensor of the ExoMars 2020 mission. This mission has strict bioburden requirements. The electromagnetic properties of several materials have been analyzed in order to study their transmission coefficient and the innovation of this project is the use of fused deposition modeling (FDM) technology as manufacturing method. Additive manufacturing is presented as a promising technology in the field of radiofrequency since it can use a wide range of polymeric materials (thermoplastics) with low transmission coefficient. Observing the electromagnetic (EM) characterization results, it was decided to manufacture a protective cover using FDM technology, because it allows control over the grounding of the instrument and facilitates the integration, cleaning and protection against impacts during the manipulation, with great versatility and low cost. Finally, the cover has been verified during the acceptance EMC tests of the flight model AMR instrument.es
dc.description.peerreviewedPreprintes
dc.description.sponsorshipThis work has received funding from the Ministerio de Econom´ıa, Industria y Competitividad (MEIC) Projects TEC2016-79214-C3-1-R, ESP2015-70184-R and ESP2017- 88930-R.es
dc.identifier.citationInternational Symposium on Electromagnetic Compatibility - EMC Europe 2019es
dc.identifier.doi10.1109/EMCEurope.2019.8872129
dc.identifier.otherhttps://ieeexplore.ieee.org/document/8872129es
dc.identifier.urihttp://hdl.handle.net/20.500.12666/759
dc.language.isoenges
dc.publisherInstitute of Electrical and Electronics Engineerses
dc.relationinfo: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.relationinfo:eu-repo/grantAgreement/MINECO//ESP2015-70184-Res
dc.relationinfo:eu-repo/grantAgreement/AEI/Plan Estatal de Investigación Científica y Técnica y de Innovación 2013-2016/ESP2017-88930-R/ES/DESARROLLO DE INSTRUMENTACION MAGNETICA PARA LA INVESTIGACION DEL SISTEMA MARCIANO Y ESTUDIO Y ANALISIS DE ANALOGOS TERRESTRES/es
dc.rights.accessRightsinfo:eu-repo/semantics/restrictedAccesses
dc.rights.licenseCopyright © 2019, IEEEes
dc.subjectPlanetary Protectiones
dc.subjectTransmission coefficientes
dc.subjectAn-isotropices
dc.subjectMagneto-resistance sensores
dc.subjectAdditive manufacturinges
dc.subjectFDMes
dc.titleDesign of a planetary protection cover for EMC testing of a spacial magnetic sensores
dc.typeinfo:eu-repo/semantics/articlees
dc.type.coarhttp://purl.org/coar/resource_type/c_6501es
dc.type.hasVersioninfo:eu-repo/semantics/publishedVersiones
dspace.entity.typePublication

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