Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwell/General Dynamics version of the space shuttle in the NASA/MSFC 14 x 14 Inch Trisonic Wind Tunnel. Static stability and control data were obtained on the delta wing booster alone (B-20) and with the delta wing orbiter (134D) mounted in various positions on the booster. Six component aerodynamic force and moment data were recorded over an angle of attack range from -10 to 24 deg at 0 and 6 deg sideslip angles and from -10 to +10 deg sideslip at 0 deg angle of attack. Mach number ranged from 0.6 to 4.96. (Author)


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    Titel :

    Space Shuttle Static Stability and Control Investigation of Nr/Gd delta Wing Booster (B-20) AND DELTA Wing Orbiter (134-D), Volume 3


    Beteiligte:
    E. C. Allen (Autor:in) / F. W. Eder (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    496 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch