Simple-1: Development stage of the data transmission system for a solid propellant mid-power rocket model

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dc.contributor.authorYarce A.
dc.contributor.authorSebastián Rodríguez J.
dc.contributor.authorGalvez J.
dc.contributor.authorGómez A.
dc.contributor.authorGarcía M.J.
dc.contributor.departmentUniversidad EAFIT. Departamento de Cienciasspa
dc.contributor.researchgroupBioiversidad, Evolución y Conservaciónspa
dc.creatorYarce A.
dc.creatorSebastián Rodríguez J.
dc.creatorGalvez J.
dc.creatorGómez A.
dc.creatorGarcía M.J.
dc.date.accessioned2021-03-23T20:06:35Z
dc.date.available2021-03-23T20:06:35Z
dc.date.issued2017-01-01
dc.description.abstractThis paper presents the development stage of a communication module for a solid propellant mid-power rocket model. The communication module was named. Simple-1 and this work considers its design, construction and testing. A rocket model Estes Ventris Series Pro II® was modified to introduce, on the top of the payload, several sensors in a CanSat form factor. The Printed Circuit Board (PCB) was designed and fabricated from Commercial Off The Shelf (COTS) components and assembled in a cylindrical rack structure similar to this small format satellite concept. The sensors data was processed using one Arduino Mini and transmitted using a radio module to a Software Defined Radio (SDR) HackRF based platform on the ground station. The Simple-1 was tested using a drone in successive releases, reaching altitudes from 200 to 300 meters. Different kind of data, in terms of altitude, position, atmospheric pressure and vehicle temperature were successfully measured, making possible the progress to a next stage of launching and analysis. © Published under licence by IOP Publishing Ltd.eng
dc.identifierhttps://eafit.fundanetsuite.com/Publicaciones/ProdCientif/PublicacionFrw.aspx?id=6871
dc.identifier.doi10.1088/1742-6596/850/1/012019
dc.identifier.issn17426596
dc.identifier.otherWOS;000437878400019
dc.identifier.otherSCOPUS;2-s2.0-85021880092
dc.identifier.urihttp://hdl.handle.net/10784/26785
dc.language.isoengeng
dc.publisherIOP PUBLISHING LTD
dc.relation.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-85021880092&doi=10.1088%2f1742-6596%2f850%2f1%2f012019&partnerID=40&md5=0e5e4c238c56c17af42ed11e22cef425
dc.rightshttps://v2.sherpa.ac.uk/id/publication/issn/1742-6596
dc.sourceJournal Of Physics: Conference Series
dc.subject.keywordAtmospheric pressureeng
dc.subject.keywordData communication systemseng
dc.subject.keywordElectric power transmissioneng
dc.subject.keywordPrinted circuit boardseng
dc.subject.keywordPropellantseng
dc.subject.keywordRocketseng
dc.subject.keywordSolid propellantseng
dc.subject.keywordCommercial off-the-shelf componentseng
dc.subject.keywordCommunication moduleseng
dc.subject.keywordDevelopment stageseng
dc.subject.keywordGround stationseng
dc.subject.keywordPrinted circuit boards (PCB)eng
dc.subject.keywordRack structureseng
dc.subject.keywordSatellite concepteng
dc.subject.keywordSoftware-defined radioseng
dc.subject.keywordSoftware radioeng
dc.titleSimple-1: Development stage of the data transmission system for a solid propellant mid-power rocket modeleng
dc.typeinfo:eu-repo/semantics/conferencePapereng
dc.typeconferencePapereng
dc.typeinfo:eu-repo/semantics/publishedVersioneng
dc.typepublishedVersioneng
dc.type.localDocumento de conferenciaspa

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