The patent application relates to a pressure activated, timed missile flight termination system for destroying a test missile after a predetermined period of flight to shorten its hazard space so that it can be used on firing ranges having a minimum amount of area. A delayed destruct sequence is initiated by pressure in the missile combustion chamber upon ignition of the missile. A pressure driven piston is compressed by the pressure created in the combustion chamber, causing it to strike a primer which initiates a delay fuse, a detonator, and a linear-shaped charge to destroy the missile.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Timed Missile Flight Termination System


    Beteiligte:
    D. B. Franz (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    UpSTAGE Missile Flight Control System

    Pearson, John L. | SAE Technical Papers | 1970



    Peacekeeper flight termination ordnance system

    Ramsey, James / Sessler, Donald / Yang, Lien | AIAA | 1995