Please use this identifier to cite or link to this item: http://hdl.handle.net/20.500.12666/897
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dc.rights.licenseCopyright © 2019 by Instituto Nacional de Técnica Aeroespacial (INTA).es
dc.contributor.authorBardera, Rafaeles
dc.contributor.authorGarcía Magariño, A.es
dc.contributor.authorSor, Suthyvannes
dc.contributor.authorUrdiales, María del Mares
dc.date.accessioned2023-11-28T10:51:20Z-
dc.date.available2023-11-28T10:51:20Z-
dc.date.issued2019-02-11-
dc.identifier.citationJournal of Spacecraft and Rockets 56(4)es
dc.identifier.issn0022-4650-
dc.identifier.otherhttps://arc.aiaa.org/doi/full/10.2514/1.A34362es
dc.identifier.urihttp://hdl.handle.net/20.500.12666/897-
dc.descriptionCopyright © 2019 by Instituto Nacional de Técnica Aeroespacial (INTA). Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-6794 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.es
dc.description.abstractThe Mars 2020 rover is the new vehicle dedicated to the Martian surface investigation. This vehicle will transport Mars Environmental Dynamic Analyzer, the new meteorological station, including two wind sensors installed in the camera mast. An experimental characterization was conducted to investigate the influence of the Mars 2020 rover in the Mars Environmental Dynamic Analyzer wind measurements at low Reynolds numbers. Wind tunnel experiments were conducted using a 1:45th scaled model in a wind tunnel specially designed for these experiments. The velocity was measured using laser Doppler anemometry. A method is proposed in this investigation to calculate a correction factor for the data measurements of wind sensors embarked on rovers dedicated to planetary exploration missions. In particular, the method was applied to wind measurements taken by Mars Environmental Dynamic Analyzer in the Mars 2020 rover using the laser Doppler anemometry measurements, and corrections up to 40% in the velocity magnitude and 23 deg in the deflection angle were found.es
dc.description.sponsorship"This investigation was funded by Spanish Ministry of Defense under the program “Termofluidodinámica” of Instituto Nacional de Técnica Aerospacial"es
dc.language.isoenges
dc.publisherAerospace Research Centrales
dc.subjectAerodynamic performancees
dc.subjectAerodynamicses
dc.subjectAeronauticses
dc.subjectAerospace engineeringes
dc.subjectAerospace scienceses
dc.subjectAirline operationses
dc.subjectAirlineses
dc.subjectAstronauticses
dc.subjectAtmospheric sciencees
dc.subjectAviationes
dc.subjectAvionicses
dc.subjectFluid dynamicses
dc.subjectMeteorologyes
dc.subjectSensorses
dc.subjectTransducerses
dc.subjectWind tunnelses
dc.titleMars 2020 Rover Influence on Wind Measurements at Low Reynolds Numberes
dc.typeinfo:eu-repo/semantics/articlees
dc.identifier.doi10.2514/1.A34362-
dc.identifier.e-issn1533-6794-
dc.contributor.funderInstituto Nacional de Técnica Aeroespacial (INTA)es
dc.description.peerreviewedPeerreviewes
dc.type.hasVersioninfo:eu-repo/semantics/acceptedVersiones
dc.rights.accessRightsinfo:eu-repo/semantics/restrictedAccesses
dc.type.coarhttp://purl.org/coar/resource_type/c_6501es
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