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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:
    D. C. Freeman (Autor:in) / R. H. Fournier (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    119 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch