During orbital maneuvers and proximity operations, a spacecraft fires its thrusters inducing plume impingement loads, heating and contamination to itself and to any other nearby spacecraft. These thruster firings are generally modeled using a combination of Computational Fluid Dynamics (CFD) and DSMC simulations. The Shuttle Plume Impingement Flight EXperiment(SPIFEX) produced data that can be compared to a high fidelity simulation. Due to the size of the Shuttle thrusters this problem was too resource intensive to be solved with DSMC when the experiment flew in 1994.


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    Titel :

    DSMC simulations of the Shuttle Plume Impingement Flight EXperiment(SPIFEX)


    Beteiligte:

    Kongress:

    Direct Simulation Monte Carlo (DSMC) Conference 2017 ; 2017 ; Santa Fe, NM, United States


    Erscheinungsdatum :

    2017-08-29


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





    A CFD/DSMC analysis of plumes and plume impingement during Shuttle /Mir docking

    Lumpkin, st E, I, Forrest / IIL, Gerald / Stuart, Philip | AIAA | 1995


    Shuttle Plume Impingement Flight Experiment (SPIFEX) - Heat flux measurements and predictions

    Rochelle, Wm. / Hughes, J. / Leahy, Kenneth et al. | AIAA | 1996


    Shuttle Plume Impingement Flight Experiment (SPIFEX) - Pressure and load plate measurements

    Fitzgerald, Steve / Machin, Ricardo / Hughes, J. et al. | AIAA | 1996


    The Load Measurement System (LMS) of the Shuttle Plume Impingement Flight Experiment

    Rocha, A. / AIAA / ASME et al. | British Library Conference Proceedings | 1996