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      Mars 2020 Rover Influence on Wind Measurements at Low Reynolds Number

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          Abstract

          The 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.

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          REMS: The Environmental Sensor Suite for the Mars Science Laboratory Rover

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            Martian Meteorology

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              Meteorology experiments: the viking mars lander

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                Author and article information

                Conference
                jsr
                Journal of Spacecraft and Rockets
                J. Spacecraft
                American Institute of Aeronautics and Astronautics
                0022-4650
                1533-6794
                08 February 2019
                July–August 2019
                : 56
                : 4
                : 1107-1113
                Affiliations
                National Institute of Aerospace Technology , Torrejón de Ardoz, Madrid 28850, Spain
                Author notes
                [*]

                Ph.D. Aerospace Engineer, Experimental Aerodynamics; barderar@ 123456inta.es .

                [†]

                Ph.D. Aerospace Engineer, Experimental Aerodynamics; garciamga@ 123456inta.es .

                [‡]

                Ph.D. Aerospace Engineer, Experimental Aerodynamics; sors@ 123456inta.es .

                [§]

                Aerospace Engineer, Experimental Aerodynamics; urdiales@ 123456inta.es .

                Article
                A34362 A34362
                10.2514/1.A34362
                693bf213-a5e2-4a1a-afa3-b6257da3ca0f
                Copyright © 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.
                History
                : 31 July 2018
                : 22 November 2018
                : 26 December 2018
                Page count
                Figures: 15, Tables: 0
                Funding
                Funded by: Spanish Ministry of Defense
                Award ID: Termofluidodinámica of INTA
                Categories
                Full-Length Papers

                Engineering,Physics,Mechanical engineering,Space Physics
                Engineering, Physics, Mechanical engineering, Space Physics

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