Abstract This research is an investigation about the possibility of using shaped charges forming high-velocity metal jets to obtain high-velocity compact elements. The particular objective here is testing rocket and space technology objects for anti-meteoroid resistance. In order to “cut off” the jet head section and obtain a compact element with a velocity of 10 km/s, it is proposed to create an axial magnetic field in the shaped charge liner before its explosion. Strengthening the magnetic field in the jet formation region during the liner collapse leads to destroying the main part of the forming shaped-charge jet. This is associated with radial dispersion of its material due to the accompanying “pumping excitation” field of powerful electromagnetic forces. In this case, it is possible to maintain the jet head section at maximum velocity. The possibility of choosing an initial magnetic field intensity has been analyzed. This is done based on numerical modeling in the framework of the two-dimensional axisymmetric problem of continuum mechanics and electrodynamics, assuming ideal conductivity of the liner material. The way of doing so is that only the head section of the jet is formed normally and its subsequent sections are scattered. As calculations showed, the goal is achieved in the case of using conical shaped charge liners with apex angles of 60° … 80° at induction of the magnetic field created in the liner at level of tenths of a tesla which is technically quite easy to implement.

    Highlights Metal shaped charge jets can be used to produce high-speed compact elements. A magnetic field can be used to “cut off” the head section of the shaped charge jet. The magnetic field increases in the jet formation region during liner collapse. Magnetic field producing in the shaped charge liner leads to the jet destruction. To obtain a high-speed element, the magnetic field induction must be about 0.2 T.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Using shaped charges with a “magnetic cut-off” for testing anti-meteoroid shields


    Beteiligte:
    Selivanov, V.V. (Autor:in) / Fedorov, S.V. (Autor:in) / Babkin, A.V. (Autor:in) / Bolotina, I.A. (Autor:in)

    Erschienen in:

    Acta Astronautica ; 180 ; 170-175


    Erscheinungsdatum :

    2020-12-12


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Hydrocode modeling of meteoroid/debris shields

    Kerr, Justin / Christiansen, Eric / Crews, Jeannne | AIAA | 1995


    NEW PROTECTION CONCEPTS FOR METEOROID / DEBRIS SHIELDS

    Thoma, K. / Wicklein, M. / Schneider, E. | British Library Conference Proceedings | 2005


    Designing space vehicle shields for meteoroid protection: A new analysis

    Swift, H.F. / Bamford, R. / Chen, R. | Elsevier | 1983


    Designing space vehicle shields for meteoroid protection - A new analysis

    Swift, H. F. / Bamford, R. / Chen, R. | NTRS | 1982