A simultaneous spin/eject mechanism was developed for aerospace applications requiring a compact, passive device which would accommodate payload support and controlled-release functions, and which would provide a highly accurate spin-ejection motion to the payload. The mechanism satisfied the requirements and is adaptable to other deployment applications.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    A simultaneous spin/eject mechanism for aerospace payloads


    Contributors:


    Publication date :

    1976-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






    Spin and eject device

    Grunditz, H. / Andersson, H. / Vik, A. et al. | British Library Online Contents | 1996


    Spin and eject device

    Grunditz, H. / Andersson, H. / Vik, A. et al. | British Library Conference Proceedings | 1996


    AUTO-EJECT CHARGING PLUG

    CHO JUNG GOO / KIM NAM IN | European Patent Office | 2024

    Free access