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    Title :

    RELIABILITY BASED DESIGN OPTIMIZATION OF A CUBESAT DE-ORBITING MECHANISM



    Conference:

    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



    Publication date :

    2012-01-01


    Size :

    12 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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