Experimental aerodynamic investigations of the configuration 4 space shuttle orbiter were conducted in the 14-inch trisonic wind tunnel during November and December 1973. Elevon, aileron, bodyflap, speedbrake, rudder effectiveness, and effects of ventral fins were investigated at angles of attack from -10 deg to 40 deg, angles of sideslip from -10 deg to +10 deg, and Mach numbers from 0.6 to 4.96. Resulting six-component static stability data and associated test information are presented. (Author)


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    Titel :

    Results of Transonic/Supersonic Static Stability Wind Tunnel Tests of an 0.004-Scale Space Shuttle Orbiter Model (0A49)


    Beteiligte:
    E. Allen (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    1199 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch