Liquid propellant and elastic behavior of boosters exhibit problem areas which should be considered in preliminary design stage; influence of propellant sloshing on stability of vehicle requires knowledge of liquid motion for various container geometries; since stability of vehicle alone is not sufficient for success of mission, magnification function of various generalized coordinates is also presented; these response functions lead way for design of swivel engine system.


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    Title :

    Interactions of structural vibrations, propellant sloshing and control frequency in booster rockets


    Additional title:

    Zum Zusammenwirken struktureller Schwingungen, Treibstoffschwappen und der Regelfrequenz bei Traegerraketen


    Contributors:
    Bauer, F. (author)

    Published in:

    Publication date :

    1965


    Size :

    15 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German




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