A review of the effects that onboard liquid may have on the dynamics of the spacecraft is given. A distinction is made between arbitrarily moving craft and spin stabilized vehicles. The modeling of rotating liquid behavior is very complicated and generally allows only predictions on the stability behavior of a spinning spacecraft. A flight experiment with a model satellite with liquid in an annular tank, during parabolic aircraft flight is described. From a filmed record of the unconstrained motion, the attitude of the satellite is reconstructed. Details of the image processsing scheme are given. The numerical simulation of the motion of the model satellite is explained. The liquid is inviscid and is assumed to move in the tank in two directions only, i.e., radial motion, is neglected. Surface tension effects are important and are fully accounted for. The angular rates of the model following a short duration torque, are presented. Plots of the liquid motion are included.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Effects of Low Bond Number Liquid Motions on Spacecraft Attitude


    Contributors:

    Publication date :

    1989


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English