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dc.rights.licenseCopyright © 2020, IEEE-
dc.contributor.authorFernández Romero, S.-
dc.contributor.authorMuñoz Rebate, I.-
dc.contributor.authorJiménez Lorenzo, María-
dc.contributor.authorPlaza Gallardo, B.-
dc.contributor.authorPoyatos Martínez, D.-
dc.contributor.authorDíaz Michelena, M.-
dc.date.accessioned2022-04-04T07:18:19Z-
dc.date.available2022-04-04T07:18:19Z-
dc.date.issued2020-06-22-
dc.identifier.citationIEEE Letters on Electromagnetic Compatibility Practice and Applications 2(2): 46-50(2020)es
dc.identifier.otherhttps://ieeexplore.ieee.org/document/9122588-
dc.identifier.urihttp://hdl.handle.net/20.500.12666/721-
dc.descriptionINSPEC Accession Number: 19976292es
dc.description.abstractThis letter addresses on the design of a planetary protection shell for performing the Electro-Magnetic Compatibility (EMC) tests of the Anisotropic Magneto-Resistance (AMR) sensor of the ExoMars mission. This mission has strict bio-burden requirements. The ElectroMagnetic (EM) properties of several materials have been investigated for measuring their transmission coefficients and the novelty of this letter is the use of Fused Deposition Modeling (FDM) technology as the production method. Additive manufacturing is presented as a promising technology in the field of radiofrequency since it can use a wide range of materials (including thermoplastics) with high and low transmission coefficient. The investigation comprises the analysis of the electromagnetic properties of several 3D printer materials in order to study their transmission coefficients. Seeing the EM characterization results, it was decided to produce a shell using FDM technology because it provides control over the grounding of the instrument and makes easier the integration, cleaning and protection against impacts during the operation, with great versatility and low cost. To finish, the shell has been proved during the acceptance EMC tests of the flight model and flight spare AMR instrument.es
dc.description.sponsorshipMinisterio de Economía, Industria y Competitividad (Grant Number: UAVE3 TEC-2016-79214-C3-1-R and MAGARES ESP2017-88930-R)es
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/ESP2017-88930-R/ES/DESARROLLO DE INSTRUMENTACION MAGNETICA PARA LA INVESTIGACION DEL SISTEMA MARCIANO Y ESTUDIO Y ANALISIS DE ANALOGOS TERRESTRES/-
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/-
dc.subjectAdditive manufacturinges
dc.subjectAn isotropic magneto-resistance sensores
dc.subjectBio-burden requirementes
dc.subjectFDMes
dc.subjectPlanetary protectiones
dc.subjectTransmission coefficientes
dc.subjectRadio frequencyes
dc.subjectMagnetospherees
dc.titleOn the Design of a Planetary Protection Shell for EMC Testing on Space Equipmentes
dc.typeinfo:eu-repo/semantics/articlees
dc.contributor.orcidFernández Romero, S. [0000-0002-7169-2222]-
dc.contributor.orcidJiménez Lorenzo, M. [0000-0003-1243-6111]-
dc.contributor.orcidPlaza Gallardo, B. [0000-0003-3615-0353]-
dc.contributor.orcidPoyatos Martínez, D. [0000-0002-3829-5110]-
dc.identifier.doi10.1109/LEMCPA.2020.3004203-
dc.identifier.e-issn2637-6423-
dc.contributor.funderAgencia Estatal de Investigación (AEI)-
dc.description.peerreviewedPeerreviewes
dc.identifier.funderhttp://dx.doi.org/10.13039/501100011033-
dc.type.hasVersioninfo:eu-repo/semantics/publishedVersion-
dc.rights.accessRightsinfo:eu-repo/semantics/restrictedAccess-
dc.type.coarhttp://purl.org/coar/resource_type/c_6501-
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