Analog computer and theoretical results are presented to show the nonlinear stability of any steady-state propellant temperature and flow in a typical nuclear rocket engine. This assurance of stability encourages design of schemes involving only propellant flow control or on-off drum controllers.


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    Title :

    Stability of nuclear rocket engine dynamics


    Contributors:
    Wiberg, D.M. (author) / Woyski, J.S. (author)

    Published in:

    NUCLEAR APPL. ; 5 , 1 ; 35-45


    Publication date :

    1968


    Size :

    11 Seiten, 6 Bilder, 1 Tabelle, 17 Quellen


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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