A test of a 0.004-scale MCR 0074 Baseline Launch Configuration Space Shuttle model was conducted in the NASA-MSFC 14 x 14-inch Trisonic Wind Tunnel (MSFC TWT 566). The objective of the test was to determine the effects of model parametric variations on aerodynamic static stability characteristics over a Mach number range from 0.6 to 4.96. Angles-of-attack from minus 10 deg to plus 10 deg at 0 deg sideslip and angles-of-sideslip from minus 10 deg to plus 10 deg at minus 5 deg, 0 deg, and plus 5 deg angle-of-attack were investigated. The basic configuration investigated was the integrated vehicle consisting of the orbiter, and external tank, and two solid rocket boosters. It was designated 03T9S3. (Author)


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    Titel :

    Aerodynamic Investigations on a 0.004 Scale Model Mcr 0074 Baseline Space Shuttle Launch Vehicle at Mach Numbers Between 0.6 and 4.96


    Beteiligte:
    P. Ramsey (Autor:in) / M. K. Robertson (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    400 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch