This paper describes a numerical simulation of the hydrodynamics within the liquid oxygen tank of the Space Shuttle External Tank during liftoff. Before liftoff, the tank is filled with liquid oxygen (LOX) to approximately 97 % full with the other 3 % containing gaseous oxygen (GOX) and helium. During liftoff, LOX is drained from the bottom of the tank, and GOX is pumped into the tank's ullage volume. There is a delay of several seconds before the GOX reaches the tank which causes the ullage pressure to decrease for several seconds after liftoff; this pressure 'slump' is a common phenomenon in rocket propulsion. When four slosh baffles were removed from the tank, the ullage gas pressure dropped more rapidly than in all previous flights. The purpose of this analysis was to determine whether the removal of the baffles could have caused the increased pressure 'slump' by changing the LOX surface dynamics. The results show that the LOX surface undergoes very high vertical accelerations (up to 5g) and, therefore, splashing almost certainly occurs. The number of baffles does not affect the surface if the same structural motion is assumed; but, the number of baffles may affect the structural motion of the tank.


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    Title :

    Liquid oxygen sloshing in space shuttle external tank


    Additional title:

    Verschuetten von Fluessigsauerstoff in Aussentank der Raumfaehre


    Contributors:

    Published in:

    AIAA-Papers ; Jul ; 1-6


    Publication date :

    1987


    Size :

    6 Seiten, 12 Bilder, 6 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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