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On the Design of a Planetary Protection Shell for EMC Testing on Space Equipment

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.contributor.funderAgencia Estatal de Investigación (AEI)
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.date.accessioned2022-04-04T07:18:19Z
dc.date.available2022-04-04T07:18:19Z
dc.date.issued2020-06-22
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.peerreviewedPeerreviewes
dc.description.sponsorshipMinisterio de Economía, Industria y Competitividad (Grant Number: UAVE3 TEC-2016-79214-C3-1-R and MAGARES ESP2017-88930-R)es
dc.identifier.citationIEEE Letters on Electromagnetic Compatibility Practice and Applications 2(2): 46-50(2020)es
dc.identifier.doi10.1109/LEMCPA.2020.3004203
dc.identifier.e-issn2637-6423
dc.identifier.funderhttp://dx.doi.org/10.13039/501100011033
dc.identifier.otherhttps://ieeexplore.ieee.org/document/9122588
dc.identifier.urihttp://hdl.handle.net/20.500.12666/721
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.rights.accessRightsinfo:eu-repo/semantics/restrictedAccess
dc.rights.licenseCopyright © 2020, IEEE
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.type.coarhttp://purl.org/coar/resource_type/c_6501
dc.type.hasVersioninfo:eu-repo/semantics/publishedVersion
dspace.entity.typePublication

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