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    Magnetic Sampler for Regolith Particles on Asteroids

    Source: Journal of Aerospace Engineering:;2018:;Volume ( 031 ):;issue: 002
    Author:
    M. Adachi
    ,
    R. Obata
    ,
    H. Kawamoto
    ,
    S. Wakabayashi
    ,
    T. Hoshino
    DOI: 10.1061/(ASCE)AS.1943-5525.0000797
    Publisher: American Society of Civil Engineers
    Abstract: A magnetic sampler for future sample return missions on asteroids was developed. The sampler had a simple configuration, consisting of a solenoid coil, direct current (DC) power supply, and switching circuit, and the sampling was conducted using the coil gun mechanism. The sampler did not require mechanical moving parts, gas, or liquid, and its control was simple; thus, it was reliable for use in a space environment. The authors analyzed the particle motion in a magnetic field on Earth and in space environments; the sampler performance was evaluated by numerical calculations on the basis of the distinct element method and experiments in air and vacuum environments. The results of numerical calculations and experiments were consistent qualitatively with the analytical calculations. The magneto-motive force and its applied time mutually affected the dynamics of particles. The magnetic interaction of particles in the magnetic field also affected the sampler performance. Moreover, the sampler performance in vacuum and a microgravity of 0.00001g was better than that on Earth owing to the absence of air drag and small gravitational force.
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      Magnetic Sampler for Regolith Particles on Asteroids

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4245055
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    contributor authorM. Adachi
    contributor authorR. Obata
    contributor authorH. Kawamoto
    contributor authorS. Wakabayashi
    contributor authorT. Hoshino
    date accessioned2017-12-30T13:03:09Z
    date available2017-12-30T13:03:09Z
    date issued2018
    identifier other%28ASCE%29AS.1943-5525.0000797.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4245055
    description abstractA magnetic sampler for future sample return missions on asteroids was developed. The sampler had a simple configuration, consisting of a solenoid coil, direct current (DC) power supply, and switching circuit, and the sampling was conducted using the coil gun mechanism. The sampler did not require mechanical moving parts, gas, or liquid, and its control was simple; thus, it was reliable for use in a space environment. The authors analyzed the particle motion in a magnetic field on Earth and in space environments; the sampler performance was evaluated by numerical calculations on the basis of the distinct element method and experiments in air and vacuum environments. The results of numerical calculations and experiments were consistent qualitatively with the analytical calculations. The magneto-motive force and its applied time mutually affected the dynamics of particles. The magnetic interaction of particles in the magnetic field also affected the sampler performance. Moreover, the sampler performance in vacuum and a microgravity of 0.00001g was better than that on Earth owing to the absence of air drag and small gravitational force.
    publisherAmerican Society of Civil Engineers
    titleMagnetic Sampler for Regolith Particles on Asteroids
    typeJournal Paper
    journal volume31
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000797
    page04017095
    treeJournal of Aerospace Engineering:;2018:;Volume ( 031 ):;issue: 002
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian