A document describes a series of models created for the determination of the probability of survival of critical spacecraft components from particle strike damage caused by hypervelocity impact of meteoroids and/or orbital debris. These models were integrated with both shield design and hypervelocity impact testing to develop adequate protection of said components to meet mission survivability requirements.


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    Title :

    Meteoroid/Orbital Debris Shield Engineering Development Practice and Procedure


    Contributors:


    Publication date :

    2011-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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