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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    Title :

    System protection requirements for resistance of meteoroid penetration damage


    Additional title:

    J Spacecraft Rockets


    Contributors:

    Published in:

    Publication date :

    1966


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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