To support focused science and engineering missions, spacecraft bus designs should minimize mass and maximize design flexibility without reducing capability. This requires a highly efficient spacecraft structure to maintain the required stiffness with a minimal mass.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Thermo-mechanical design of honeycomb panel with fully-potted inserts used for spacecraft design


    Contributors:
    Boudjemai, A. (author) / Bouanane, M.H. (author) / Mankour, A. (author) / Salem, H. (author) / Hocine, R. (author) / Amri, R. (author)


    Publication date :

    2013-06-01


    Size :

    1342187 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Methods for installation of potted inserts having a latch mechanism

    LACONTE RICHARD J | European Patent Office | 2017

    Free access

    STRUCTURAL INSERTS FOR HONEYCOMB STRUCTURES

    HOLEMANS PETER | European Patent Office | 2017

    Free access

    STRUCTURAL INSERTS FOR HONEYCOMB STRUCTURES

    PETER HOLEMANS | European Patent Office | 2016

    Free access

    STRUCTURAL INSERTS FOR HONEYCOMB STRUCTURES

    HOLEMANS PETER | European Patent Office | 2021

    Free access

    STRUCTURAL INSERTS FOR HONEYCOMB STRUCTURES

    European Patent Office | 2020

    Free access