Erosive effect is greater in slow burning propellants than in fast burning ones; existence of apparent "threshold velocity for erosion" is tentatively attributed to failure of onedimensional idealization to represent true flow conditions obtaining at fore end of grain; more comprehensive studies of phenomenon required in order to resolve threshold velocity question. (formerly Am Rocket Soc -- J)


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    Titel :

    Erosive burning of some composite solid propellants


    Weitere Titelangaben:

    Jet Propulsion


    Beteiligte:
    Green, Jr., L. (Autor:in)

    Erschienen in:

    Jet Propulsion ; 24 , n 1


    Erscheinungsdatum :

    1954


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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