Future NASA missions require long, ultra-lightweight booms to enable solar sails, large sunshields, and other gossamer-type spacecraft structures. The space experiment discussed in this paper will flight validate the non-traditional ultra lightweight rigidizable, inflatable, isogrid structure utilizing graphite shape memory polymer (GR/SMP) called UltraBoom(TradeMark). The focus of this paper is the analysis of the 3-m ground test article. The primary objective of the mission is to show that a combination of ground testing and analysis can predict the on-orbit performance of an ultra lightweight boom that is scalable, predictable, and thermomechanically stable.


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    Titel :

    Preliminary Analysis of the 30-m UltraBoom Flight Test


    Beteiligte:
    Agnes, Gregory S. (Autor:in) / Abelson, Robert D. (Autor:in) / Miyake, Robert (Autor:in) / Lin, John K. H. (Autor:in) / Welsh, Joe (Autor:in) / Watson, Judith J. (Autor:in)

    Kongress:

    46th Structural Dynamics and Materiels Conference ; 2005 ; Austin, TX


    Erscheinungsdatum :

    2005-04-18


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




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