An analysis of pressure and strain-gage data from space shuttle wind tunnel test IA119 and IA138 was performed to define the influence on aerodynamic characteristics resulting from the main propulsion system and solid rocket booster plumes. Aerodynamic characteristics of each of the elements, the components and total vehicle of the space shuttle vehicle during ascent flight was considered. Pressure data were obtained over the aft portions of the space shuttle wind tunnel model in addition to wing and elevon gage data.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space shuttle plume/simulation application


    Beteiligte:
    Boyle, W. (Autor:in) / Conine, B. (Autor:in) / Bell, G. (Autor:in)

    Erscheinungsdatum :

    15.05.1979


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Space Shuttle Plume/Simulation Application

    W. Boyle / B. Conine / G. Bell | NTIS | 1979





    Space Shuttle Plume and Plume Impingement Study

    Tevepaugh, J. A. / Penny, M. M. | NTRS | 1977