Variable thrust from rocket power plants has not been generally available except in large increments obtained from firing one or more thrust chambers; burning rates of solid fuels are not readily controllable; with liquid propellants, control is more easily accomplished; throttling thrust chamber control using liquid propellants should considerably augment utility of rocket power plants in piloted as well as possibly pilotless aircraft.


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    Titel :

    Throttling thrust-chamber control


    Weitere Titelangaben:

    Am Rocket Soc -- J


    Beteiligte:
    Meyer, M. (Autor:in)


    Erscheinungsdatum :

    1951


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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