The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determine the longitudinal and lateral-directional aerodynamic characteristics of a winged single-state-to-orbit vehicle was investigated. The model was tested over a Mach number range from 0.3 to 4.63 for an angle-of-attack range from 4 to 30 D at both 0 and 5 D sideslip.


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    Title :

    Static Aerodynamic Characteristics of a Winged Single-Stage-to-Orbit Vehicle at Mach Numbers from 0.3 to 4.63


    Contributors:

    Publication date :

    1978


    Size :

    119 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English