The Sloshsat FLEVO project has an Investigators Working Group which prepared orbital experiments on the behaviour of liquid in spacecraft. These are to be performed with a dedicated small satellite, of about 90 kg empty weight and about 34 kg of water in a 87 litre tank. The spacecraft dynamics are simulated by SMS, the Sloshsat Motion Simulator. SMS predictions and those generated by a computational fluid dynamic (CFD) simulation are compared for an example.


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    Titel :

    Simulation of Liquid Dynamics Onboard Sloshsat FLEVO


    Beteiligte:

    Erscheinungsdatum :

    1999


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Models for Liquid Impact Onboard Sloshsat FLEVO

    J. P. B. Vreeburg / D. J. Chato | NTIS | 2000


    Models for liquid impact onboard Sloshsat FLEVO

    Vreeburg, Jan / Chato, David | AIAA | 2000


    Models for Liquid Impact Onboard Sloshsat FLEVO

    Vreeburg, Jan P. B. / Chato, David J. | NTRS | 2000



    Simulation of Liquid Dynamics Onboard Sloshat FLEVO

    Vreeburg, J. P. B. / University of New Mexico; School of Engineering; Institute for Space and Nuclear Power Studies | British Library Conference Proceedings | 1999