Results of an experimental aerodynamic investigation of the H-33 space orbiter are presented. The investigation was undertaken to determine static aerodynamic characteristics of the orbiter at a Mach number of 0.17. These data were determined by employing a 1/25 scale model of the orbiter for pitch and yaw variations of -4 degrees to 24 degrees to 15 degrees, respectively. Investigations were conducted in the 7 - by - 10 foot wind tunnel.


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    Title :

    Space shuttle: Basic subsonic static aerodynamic characteristics for Grumman H-33 orbiter configuration (M equals 0.17)


    Contributors:
    Jung, W. (author) / Carlucci, F. (author)

    Publication date :

    1971-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :