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    Titel :

    RELIABILITY BASED DESIGN OPTIMIZATION OF A CUBESAT DE-ORBITING MECHANISM



    Kongress:

    Conference; 12th, Aviation technology, integration and operations; ATIO conference and 14th AIAA/ISSM; includes 14th AIAA/ISSMO multidisciplinary analysis and optimization conference Indianapolis ; 2012 ; Indianopolis, IN



    Erscheinungsdatum :

    01.01.2012


    Format / Umfang :

    12 pages


    Anmerkungen:

    Includes bibliographical references and index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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