The capability of an Ultra Distributed Energy Store System (UDESS) powered electromagnetic launcher (EM) is experimentally assessed. The UDESS system was developed specifically to address the velocity speed limit seen in plasma armature EM launchers. Metal armature launch packages were also developed and tested to assess the usefulness of the UDESS concept for low velocity applications.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hypervelocity Launcher for Aerothermodynamic Experiments


    Beteiligte:

    Erscheinungsdatum :

    1995-07-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Hypervelocity Launcher Design

    K. Seifert | NTIS | 1976


    Applications of the ram accelerator to hypervelocity aerothermodynamic testing

    BRUCKNER, A. / KNOWLEN, C. / HERTZBERG, A. | AIAA | 1992


    Applications of the ram accelerator to hypervelocity aerothermodynamic testing

    Bruckner, A. P. / Knowlen, C. / Hertzberg, A. | NTRS | 1992


    Aerothermodynamic Reentry Flight Experiments Expert

    Muylaert, J. / Walpot, L. / Ottens, H. et al. | British Library Conference Proceedings | 2007