To extend knowledge of metallicsolid combustion in solid propellant rockets, metal additive behavior during actual propellant burning was investigated; alumina size distributions were obtained for coarse and fine oxidizer composite propellant burning in nitrogen atmosphere over pressure range from atmospheric to 500 psi; amount of additive agglomeration was higher for coarse oxidizer propellant and decreased with increasing pressure to 0.3 power over range from atmospheric to 250 psi; experimental findings of critical aluminum diameter required for agglomeration were in agreement with calculated data.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Alumina size distributions from high-pressure composite solid-propellant combustion


    Weitere Titelangaben:

    AIAA J


    Beteiligte:

    Erschienen in:

    AIAA Journal ; 2 , n 10 ; p 1754-1760


    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :