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    Shape of Deployable Membrane Reflectors

    Source: Journal of Aerospace Engineering:;1998:;Volume ( 011 ):;issue: 003
    Author:
    C.-Y. Lai
    ,
    Z. You
    ,
    S. Pellegrino
    DOI: 10.1061/(ASCE)0893-1321(1998)11:3(73)
    Publisher: American Society of Civil Engineers
    Abstract: The shape and stress distribution in the new Collapsible Rib-Tensioned Surface reflector are investigated both analytically and experimentally. A methodology is established for the preliminary design of symmetric reflectors of given aperture, focal length, and target root-mean-square (RMS) error, by extending form-finding methods originally developed for membrane roof covers. The concepts of a reference surface and of an equilibrium surface are introduced, and algorithms are developed to compute these surfaces and their associated RMS error. Then, the cutting pattern for making the membrane is computed and the RMS error of the actual surface is predicted. Estimates are made of the RMS error of reflectors with apertures of 1, 3, 5, and 10 m, with 6, 12, and 24 ribs. Measurements of prestress and shape in a one-sixth sector of a 1 m diameter reflector with 6 ribs are compared with predictions obtained from the computational study. In the central part of the gore, about half of the total surface, the average error on prestress is 22% whereas the shape has an RMS error of 0.7 mm, better than predicted.
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      Shape of Deployable Membrane Reflectors

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    http://yetl.yabesh.ir/yetl1/handle/yetl/44877
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    contributor authorC.-Y. Lai
    contributor authorZ. You
    contributor authorS. Pellegrino
    date accessioned2017-05-08T21:15:57Z
    date available2017-05-08T21:15:57Z
    date copyrightJuly 1998
    date issued1998
    identifier other%28asce%290893-1321%281998%2911%3A3%2873%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44877
    description abstractThe shape and stress distribution in the new Collapsible Rib-Tensioned Surface reflector are investigated both analytically and experimentally. A methodology is established for the preliminary design of symmetric reflectors of given aperture, focal length, and target root-mean-square (RMS) error, by extending form-finding methods originally developed for membrane roof covers. The concepts of a reference surface and of an equilibrium surface are introduced, and algorithms are developed to compute these surfaces and their associated RMS error. Then, the cutting pattern for making the membrane is computed and the RMS error of the actual surface is predicted. Estimates are made of the RMS error of reflectors with apertures of 1, 3, 5, and 10 m, with 6, 12, and 24 ribs. Measurements of prestress and shape in a one-sixth sector of a 1 m diameter reflector with 6 ribs are compared with predictions obtained from the computational study. In the central part of the gore, about half of the total surface, the average error on prestress is 22% whereas the shape has an RMS error of 0.7 mm, better than predicted.
    publisherAmerican Society of Civil Engineers
    titleShape of Deployable Membrane Reflectors
    typeJournal Paper
    journal volume11
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1998)11:3(73)
    treeJournal of Aerospace Engineering:;1998:;Volume ( 011 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian