This paper presents a concept for striking distance performance improvement of the GROM/PIORUN Man-Portable Air-Defence System rocket missiles by increasing the rated diameter of the rocket missile propulsion system and its fuel charge weight. A mathematical and physical model of the GROM rocket missile was designed and its enhanced propulsion system was simulated in a computer environment. The computer simulation results were displayed on plot charts.


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    Titel :

    A Concept for Striking Range Improvement of the GROM/PIORUN Man-Portable Air-Defence System


    Beteiligte:
    Krzysztof MOTYL (Autor:in) / Mirosław MAKOWSKI (Autor:in) / Bogdan ZYGMUNT (Autor:in) / Zbigniew PUZEWICZ (Autor:in) / Janusz NOGA (Autor:in)


    Erscheinungsdatum :

    2017




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt





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