Report discusses numerical simulations of flow of air about integrated space shuttle (complete space shuttle assembly including orbiter, solid rocket boosters, and external tank) in ascent. Updated version of report described in "Computed Flow About The Integrated Space Shuttle" (ARC-12685). Goal of studies to improve understanding of, and ability to predict how integrated space shuttle performs during both nominal and aborted ascent under various conditions.


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    Titel :

    Computed Flow About The Integrated Space Shuttle, Revisited


    Beteiligte:
    Buning, P. G. (Autor:in) / Obayashi, S. (Autor:in) / Steger, J. L. (Autor:in) / Chiu, I. T. (Autor:in) / Martin, F. W., Jr. (Autor:in) / Meakin, R. L. (Autor:in) / Rizk, Y. M. (Autor:in) / Yarrow, M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1996-04-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Computed Flow About The Integrated Space Shuttle

    Buning, P. G. / Chiu, I. T. / Obayashi, S. et al. | NTRS | 1991


    Shuttle entry guidance revisited

    Mease, Kenneth D. / Kremer, Jean-Paul | NTRS | 1992


    Shuttle entry guidance revisited

    MEASE, KENNETH / KREMER, JEAN-PAUL | AIAA | 1992