This report describes the results of an experimental program conducted by Physics International to develop a high-performance light-gas to launch projectiles. With this launcher the flight dynamics of re-entry vehicles could be studied to obtain erosion and ablation data in a cost-effective laboratory environment. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hypervelocity Launcher Design


    Beteiligte:
    K. Seifert (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    164 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hypervelocity Launcher for Aerothermodynamic Experiments

    Scholz, Timothy J. / Bauer, David P. | NTRS | 1995


    The MK II UTIAS Implosion-Driven Hypervelocity Launcher design analysis

    Dawson, V. C. D. / Waser, R. A. / Oakes, D. O. | TIBKAT | 1970


    Development of a Linear Implosion-driven Hypervelocity Launcher

    Loiseau, Jason / Huneault, Justin / Higgins, Andrew J. | Tema Archiv | 2013