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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    J Aerospace Sciences


    Contributors:

    Published in:

    Publication date :

    1962


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Analysis of booster-vehicle liquid propellant slosh stability duringascent-to-orbit

    MORTON, BLAISE / ELGERSMA, MICHAEL / PLAYTER, ROBERT | AIAA | 1990




    Frozen propellant - A booster concept

    Staylor, W. F. | NTRS | 1971


    Solid propellant flaw ballistic structural analysis

    FRANCIS, E. / FORD, E. | AIAA | 1984