The topics covered include the following: a test of a Space Shuttle model with various base enhancements intended to help reduce the drag of the Shuttle in the landing configuration; further tests conducted using a Shuttle model to explore base drag improvement techniques; testing of parafoils having different airfoil shapes and line lengths; a study of ground effects on a Shuttle model; and three dimensional velocity profiles in the wake aft of the Space Shuttle were determined to study the effects of wake velocities on the Orbiter drag chute.


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    Titel :

    Wind tunnel testing and research


    Beteiligte:
    Nicks, Oran W. (Autor:in)

    Erscheinungsdatum :

    1993-11-15


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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