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.


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    Titel :

    A simultaneous spin/eject mechanism for aerospace payloads


    Beteiligte:
    Palmer, G. D. (Autor:in) / Banks, T. N. (Autor:in)


    Erscheinungsdatum :

    01.07.1976


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






    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


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