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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Frangible Tube Energy Dissipation


    Contributors:

    Publication date :

    1964


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Frangible tube energy dissipation Patent

    Hathaway, M. E. / Mcgehee, J. R. / Zavada, E. J. | NTRS | 1964



    Design of a Frangible Laminated Composite Launch Tube Closure

    Wang, W. T. / Wu, J. H. / Kam, T. Y. et al. | British Library Conference Proceedings | 1999


    OMNIDIRECTIONAL FRANGIBLE JOINT

    KOSSAR CHAD STUART / YEOMANS BRADLEY / GRUBB MATTHEW | European Patent Office | 2018

    Free access

    Valve with frangible fitting

    WISE RANDY S / WOLF DENNIS A | European Patent Office | 2023

    Free access