An energy-absorbing countermass for a shoulder-launched rocket weapon is provided. The energy-absorbing countermass is to be placed behind a rocket round in the launch tube. The device has a center cylindrical section formed using a crushable aluminum honeycomb material. A lightweight piston is attached to the forward end of the center section and a mass mechanism is attached to the rearward end. The mass mechanism is a cylindrical enclosure having opening leaves. An envelope containing frangible mass is located inside the enclosure. When a rocket round is fired, the piston compresses the crushable material and at the end of the compression stroke actuates the release of the frangible mass material. The result is that the exhaust blast of the rocket round is sufficiently alternate to allow firing of a rocket weapon inside a bunker or other structure.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Energy Absorbing Countermass for Shoulder-Launched Rocket Weapon


    Beteiligte:
    M. Sanford (Autor:in) / T. A. DelGuidice (Autor:in)

    Erscheinungsdatum :

    2000


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Shoulder-Launched, Multiple-Purpose Assault Weapon

    M. M. Canaday / F. N. Watson | NTIS | 1995


    Shoulder- Launched Multi-Purpose Assault Weapon

    F. W. Watson / W. M. Canaday | NTIS | 1996


    Shoulder - Launched Multi-Purpose Assault Weapon

    M. M. Canaday / F. W. Watson | NTIS | 1997



    Guided Rocket Weapon

    P. V. Morozov | NTIS | 1982