Seven different ablative materials have been tested behind Thiokol TOMAHAWK rocket motors. The maximum erosion, erosion patterns, and the mass loss of the samples have been determined from these tests. In addition, time-dependent temperature profiles were measured in four of the test samples during firing. From these data, local ablation rates for the materials were determined (DePo)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Comparison of ablative materials in a solid rocket motor flow field


    Weitere Titelangaben:

    Vergleich waermeabsorbierender werkstoffe im Stroemungsfeld eines Festtreibstoff-Raketenantriebes


    Beteiligte:
    Henderson, J.B (Autor:in) / Anderson, L.P. (Autor:in) / Moore, G.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1979


    Format / Umfang :

    38 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch





    Shuttle solid rocket motor nozzle alternate ablative evaluation

    Powers, L. B. / Bailey, R. L. / Morrison, B. H. | NTRS | 1981


    Shuttle solid rocket motor nozzle alternate ablative evaluation

    POWERS, L. / BAILEY, R. / MORRISON, B. | AIAA | 1981



    Nanocomposite Rocket Ablative Materials: Processing, Microstructure, and Performance

    Koo, Joseph / Stretz, Holly / Weispfenning, Jon et al. | AIAA | 2004