Wind tunnel test data for the modified space shuttle vehicle orbiter is documented. Tests were made at various elevon settings and additionally in wing off/bodyflap off configuration at angles of attack from -5 to 42.5 degrees at zero yaw. Data obtained on high hypersonic longitudinal and lateral directional stability and control characteristics of the updated SSV configuration in an initially diatomic medium are included. (Author)


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    Title :

    Results of Investigation on an 0.004-Scale 140C Modified Configuration Space Shuttle Vehicle Orbiter Model (74-0) in the NASA/Langley Research Center Hypersonic Nitrogen Tunnel (OA89)


    Contributors:

    Publication date :

    1975


    Size :

    66 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English