NASA's Aeroassist Flight Experiment (AFE) vehicle will be deployed from the Space Shuttle Orbiter in 1994 to make a data-gethering aeropass through the upper atmosphere before returning to orbit for Shuttle pickup. An axisymmetric, chemically-reacting viscous shock-layer code is presently used to calculate AFE heating rates which automatically accounts for the viscous-inviscid interaction and entropy layer-swallowing effects which are ignored by the conventional boundary-layer methods. Results are presented for the stagnation-point heating of the current AFE baseline trajectory.


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    Titel :

    Flight stagnation-point heating calculations on Aeroassist Flight Experiment vehicle


    Beteiligte:
    Hamilton, H. H., II (Autor:in) / Gupta, Roop N. (Autor:in) / Jones, Jim J. (Autor:in)


    Erscheinungsdatum :

    1991-02-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Flight stagnation-point heating calculations on Aeroassist Flight Experiment vehicle

    HAMILTON, H. H. / GUPTA, ROOP N. / JONES, JIM J. | AIAA | 1991



    Aeroassist Flight Experiment (AFE)

    P. M. Siemers | NTIS | 1988


    Aeroassist Flight Experiment (AFE)

    Siemers, Paul M., III | NTRS | 1988


    The Aeroassist Flight Experiment

    Walberg, G. D. / Siemers, P. M., III / Calloway, R. L. et al. | NTRS | 1987