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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    Titel :

    Meteoroid/Orbital Debris Shield Engineering Development Practice and Procedure


    Beteiligte:


    Erscheinungsdatum :

    01.04.2011


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





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