Shock absorber assemblies are associated with the landing gear system of an aerial vehicle to enable landing of the vehicle on the earth's surface after returning from a space flight. Frangible tubular members are longitudinally disposed in relation to the moving vehicle. (Author)


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    Titel :

    Frangible Tube Energy Dissipation


    Beteiligte:
    J. R. McGhehee (Autor:in) / M. E. Hathaway (Autor:in) / E. J. Zavada (Autor:in)

    Erscheinungsdatum :

    1964


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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