A payload retention concept that may be utilized on Space Shuttle missions is investigated. This concept appears to embody all the desirable features for the very demanding requirements for space flight. Desirable features include light weight, low cost, high reliability, excellent load distribution, versatility, and insensitivity to critical alignment.


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    Titel :

    STS payload retention system concept


    Beteiligte:
    Clark, K. H. (Autor:in)

    Erscheinungsdatum :

    01.09.1982


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    STS Payload Retention System Concept

    K. H. Clark | NTIS | 1982


    Payload retention device

    Monford, Leo G., Jr. | NTRS | 1992


    AIRCRAFT PAYLOAD RETENTION SYSTEM FOR INTERIOR LOADS

    STILLE BRANDON L | Europäisches Patentamt | 2017

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