Method whereby sloshing stability of booster, with arbitrary number of fuel tanks, may be determined by inspection; means of eliminating slosh instability by employing accelerometer feedback is investigated; scheme has advantage of reducing weight penalty incurred by use of baffles to damp sloshing motion; rational determination of parameters previously obtained by computer simulation is possible.


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    Titel :

    Analysis of liquid-propellant mode stability of multitank ballistic booster vehicle


    Weitere Titelangaben:

    J Aerospace Sciences


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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