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    Titel :

    An effect of oxidizer particle size on combustion stability in composite propellants


    Beteiligte:

    Kongress:

    36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ; 2000 ; Las Vegas , NV , U.S.A.



    Erscheinungsdatum :

    01.01.2000



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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