All large spacecraft are susceptible to impacts by meteoroids and orbiting space debris. These impacts occur at extremely high speed and can damage flight-critical systems, which can in turn lead to a catastrophic failure of the spacecraft. Therefore, the design of a spacecraft for a long-duration mission must take into account the possibility of such impacts and their effects on the spacecraft structure and on all of its exposed subsystems components. The work performed under the contract consisted of applied research on the effects of meteoroid/space debris impacts on candidate materials, design configurations, and support mechanisms of long term space vehicles. Hypervelocity impact mechanics was used to analyze the damage that occurs when a space vehicle is impacted by a micrometeoroid or a space debris particle. An impact analysis of over 500 test specimens was performed to generate by a hypervelocity impact damage database.


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    Titel :

    Hypervelocity Impact Physics


    Beteiligte:
    W. P. Schonberg (Autor:in) / A. J. Bean (Autor:in) / K. Darzi (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    336 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Schonberg, William P. / Bean, Alan J. / Darzi, Kent | NTRS | 1991




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