Analytical technique is developed to estimate spacecraft component and system protection requirements for resistance of meteoroid penetration damage for any interplanetary mission; model that describes characteristics and distributions of meteoroids in planetary, asteroid belt, and interplanetary space regions is applied to selected Jupiter orbital mission, and corresponding meteoroid flux-intensity profile is shown and used to estimate protection requirement; armor requirement for conceptual heat-rejection radiator system evaluated for various interplanetary missions is discussed.


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    Titel :

    System protection requirements for resistance of meteoroid penetration damage


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Volkoff, J.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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