Tests were conducted in the NASA/LaRC 8 foot transonic wind tunnel from March 26 through 31, 1976. The model was a 0.015 scale SSV Orbiter with forebody modifications to simulate slight reductions in the reusable surface insulation (RSI) thickness. Six component aerodynamic force and moment data were obtained at Mach numbers from 0.35 to 1.20 over an angle of attack range from -2 deg to 20 deg at sideslip angles of 0 deg and 5 deg. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Transonic Stability and Control Characteristics of a 0.015 Scale Model 69-0 of the Space Shuttle Orbiter with Forebody Rsi Modification in the NASA/LARC 8 Foot Tpt (LA72)


    Beteiligte:
    J. W. Ball (Autor:in) / C. R. Edwards (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    155 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch