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    CONTOUR Dust Shield Performance

    Source: Journal of Aerospace Engineering:;2001:;Volume ( 014 ):;issue: 004
    Author:
    Roberto A. Osegueda
    ,
    Cesar J. Carrasco
    ,
    Miguel Orozco
    ,
    John Eftis
    ,
    Edward Reynolds
    ,
    Ted G. Sholar
    DOI: 10.1061/(ASCE)0893-1321(2001)14:4(147)
    Publisher: American Society of Civil Engineers
    Abstract: The Comet Nucleus Tour (CONTOUR) is one of NASA's Discovery series missions in which a single spacecraft will be launched in July 2002 to journey to the coma of comets Encke and Schwassmann-Wachmann-3 at velocities of 28.2 and 14 km/s, respectively. A multishock bumper dust shield with four ceramic fabric bumpers and a Kevlar-based rear wall, normally aligned to the dust velocity field vector, will provide the protection. Various configurations of the prototype shield were shot with surrogate nylon particles of various diameters at about 7 km/s to determine empirical ballistic limit equations. The performance is scaled to flyby velocities and comet dust particles using laws of momentum and kinetic energy and is related to the expected comets' dust fluence to determine flyby distances from the nuclei for a desired level of reliability. Empirical damage models to predict the size of the holes and mass loss of each layer are developed from measurements of the damage on the prototype targets. For small dust particles, a shield erosion model is assumed to only affect the first bumper. The damage and erosion models are incorporated into a Monte Carlo probabilistic simulation that predicts the shield damage and the probability of no penetration of the shield. This paper describes the methodology to evaluate the shield performance.
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      CONTOUR Dust Shield Performance

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    https://yetl.yabesh.ir/yetl1/handle/yetl/44950
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    contributor authorRoberto A. Osegueda
    contributor authorCesar J. Carrasco
    contributor authorMiguel Orozco
    contributor authorJohn Eftis
    contributor authorEdward Reynolds
    contributor authorTed G. Sholar
    date accessioned2017-05-08T21:16:04Z
    date available2017-05-08T21:16:04Z
    date copyrightOctober 2001
    date issued2001
    identifier other%28asce%290893-1321%282001%2914%3A4%28147%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44950
    description abstractThe Comet Nucleus Tour (CONTOUR) is one of NASA's Discovery series missions in which a single spacecraft will be launched in July 2002 to journey to the coma of comets Encke and Schwassmann-Wachmann-3 at velocities of 28.2 and 14 km/s, respectively. A multishock bumper dust shield with four ceramic fabric bumpers and a Kevlar-based rear wall, normally aligned to the dust velocity field vector, will provide the protection. Various configurations of the prototype shield were shot with surrogate nylon particles of various diameters at about 7 km/s to determine empirical ballistic limit equations. The performance is scaled to flyby velocities and comet dust particles using laws of momentum and kinetic energy and is related to the expected comets' dust fluence to determine flyby distances from the nuclei for a desired level of reliability. Empirical damage models to predict the size of the holes and mass loss of each layer are developed from measurements of the damage on the prototype targets. For small dust particles, a shield erosion model is assumed to only affect the first bumper. The damage and erosion models are incorporated into a Monte Carlo probabilistic simulation that predicts the shield damage and the probability of no penetration of the shield. This paper describes the methodology to evaluate the shield performance.
    publisherAmerican Society of Civil Engineers
    titleCONTOUR Dust Shield Performance
    typeJournal Paper
    journal volume14
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2001)14:4(147)
    treeJournal of Aerospace Engineering:;2001:;Volume ( 014 ):;issue: 004
    contenttypeFulltext
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    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