Space vehicle wall concept is presented in which self-sealing feature is incorporated into multisheet wall structure to give configuration with high penetration resistance and self-sealing capability which minimizes fluid leakage from pressurized space vehicle compartments due to leak-provoking damage resulting from impacts by meteroric particles; best configuration tested employed foaming resin activated by catalyst on impact to produce volume increase and seal puncture; weight estimates suggest that structure should produce significant weight saving for mission durations exceeding few months.


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    Titel :

    Combined system concept for control of meteoroid hazard to space vehicles


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    D'Anna, P.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :