One aspect of the present invention involves a hold-down and release mechanism (“HDRM”) that includes a hold-then-release mechanism configured to hold an element until the hold-then-release mechanism is commanded to release the element; and an integral sensor configured to sense an amount of a parameter of interest associated with the HDRM and to communicate the sensed amount of the parameter of interest to a receiving device. The parameter of interest comprises one of tensile preload, temperature, vibration, shock, and time from application of an HDRM firing current to HDRM release of the element.


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    Titel :

    HOLD DOWN RELEASE MECHANISM WITH INTEGRAL SENSING


    Beteiligte:
    NOVOTNEY DAVID (Autor:in) / KACZYNSKI GEOFF (Autor:in) / BOUCHER CRAIG (Autor:in)

    Erscheinungsdatum :

    26.07.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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