The test facility presented herein uses a groundbased rocket combustor to test the durability of new ceramic composite and metallic materials in a rocket engine thermal environment. A gaseous H2/02 rocket combustor (essentially a ground-based rocket engine) is used to generate a high temperature/high heat flux environment to which advanced ceramic and/or metallic materials are exposed. These materials can either be an integral part of the combustor (nozzle, thrust chamber etc) or can be mounted downstream of the combustor in the combustor exhaust plume. The test materials can be uncooled, water cooled or cooled with gaseous hydrogen.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A Combustion Research Facility for Testing Advanced Materials for Space Applications


    Beteiligte:

    Kongress:

    AIAA Aerospace Sciences Meeting and Exhibit ; 2003 ; Reno, NV, United States


    Erscheinungsdatum :

    06.01.2003


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    A Combustion Research Facility for Testing Advanced Materials for Space Applications

    Bur, M. J. / AIAA | British Library Conference Proceedings | 2003



    An advanced combustion research facility for validating computational fluid-dynamics codes

    Bullard, J. B. / Hurley, C. D. / Eccles, N. C. et al. | British Library Conference Proceedings | 1991


    Advanced Titus: A Facility for Materials Sciences Experiments in Space

    Naehle, R. et al. | British Library Online Contents | 1996


    Advanced Titus: A Facility for Materials Sciences Experiments in Space

    Naehle, R. / European Space Agency | British Library Conference Proceedings | 1996