Three basic areas for possible application of fluidic control to rocket engine subsystems were identified and six subsystem configurations were analyzed for study. Results provide indication of tradeoffs involved between conventional and fluidic regulators and should be of interest to control and applications engineers who need to make similar analyses.


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    Titel :

    Fluidic pressure regulators


    Beteiligte:
    Mangion, C. (Autor:in) / Miller, W. (Autor:in)

    Erscheinungsdatum :

    1972-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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