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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    Title :

    Throttling thrust-chamber control


    Additional title:

    Am Rocket Soc -- J


    Contributors:
    Meyer, M. (author)


    Publication date :

    1951


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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