Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module with deployed heat shield impact attenuation system


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Water pressure and accelerations during landing of a dynamic model of the Apollo spacecraft with a deployed-heat-shield impact-attenuation system


    Contributors:

    Publication date :

    1968-03-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :