The mast has an elementary structural unit (10) including a lower platform (13) and an upper platform (12), where the platforms are parallel to a plane (YZ) orthogonal to a longitudinal deployment axis (X). The structural unit includes stages stacked above one another parallel to the longitudinal deployment axis. Each stage includes three longitudinal flexible tape-springs (11), where each tape-spring includes upper and lower ends fixed on the upper and lower platforms, respectively. The tape-springs are identical and of the same length.


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    Titel :

    MAT DEPLOYABLE A DEPLOIEMENT SPONTANE AUTONOME ET SATELLITE COMPORTANT AU MOINS UN TEL MAT


    Beteiligte:
    GUINOT FRANCOIS (Autor:in) / FALZON FREDERIC (Autor:in) / DUCARNE JULIEN (Autor:in)

    Erscheinungsdatum :

    2017-01-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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