The development of the longitudinal restraint mechanism for the Army's Patriot missile system is reviewed. The initial design was an ordnance pin puller with a shear plane. Because of reliability problems and a desire to reduce cost, a fly-away restraint mechanism was chosen. After being manually unlocked, the restraint pin disengages the missile during launch by missile motion.


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    Titel :

    Fly-away restraint pin mechanism for the Army's PATRIOT missile system


    Beteiligte:
    Knight, F. W. (Autor:in)


    Erscheinungsdatum :

    1977-04-28


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :