Unstable combustion in liquid propellant rocket engines is discussed with reference to research conducted at Purdue Univ; unstable combustion in solid propellant rocket engine is considered and investigations conducted for determining influence of large number of parameters on acoustic instability reviewed; effects of following parameters -- shape of flow channel, mean combustion pressure, propellant temperature prior to ignition, length-to-port-diameter ratio of propellant grain, metal casing, oxidizer in composite propellants and scaling of rocket motors.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Unstable burning in solid and liquid propellant rocket motors


    Weitere Titelangaben:

    Raketentechnik u Raumfahrtforschung


    Beteiligte:
    Osborn, J.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    15 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Erosive burning in solid propellant rocket motors

    AYRIS, J. / PETROVIC, S. | AIAA | 1990


    Unstable burning in solid propellent rocket motors

    Trubridge, G.F.P. | Engineering Index Backfile | 1965


    Solid propellant rocket motors

    Smith, E.T.B. | Engineering Index Backfile | 1957