Information on a tank slosh model for Peacekeeper missiles is given in viewgraph form. Allowable vehicle errors for nose cone ejection clearance, vehicle maneuver sloshing problems, slosh/moment prediction, slosh surface specification, code validation, experimental model-computational model comparison and the propellant storage assembly are covered.


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    Title :

    Peacekeeper tank slosh model


    Contributors:


    Publication date :

    1987-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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