Real reentry flight experiments and extended investigations within different plasma wind tunnel test facilities have led to a fundamental understanding of the complex physical and chemical material surface interaction phenomena with the high enthalpy plasma flow field during atmospheric reentry. Using a newly developed two-layer coating system based on yttrium silicates, C/C-SiC have proven to be high erosion/oxidation resistance which can be improved significantly. Even under extreme thermal loads C/C-SiC showed no catastrophic failure but a controlled smooth and steady surface recession.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Reentry flight and ground testing experience with hot structures of C/C-SiC material


    Beteiligte:
    Hald, H. (Autor:in) / Ullmann, T. (Autor:in)


    Erscheinungsdatum :

    2003


    Format / Umfang :

    10 Seiten, 14 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Reentry Flight and Ground Testing Experience with Hot Structures of C/C-SiC Material

    Hald, H. / Ullmann, T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003




    Reentry vehicle flight testing and recovery techniques

    RIGALI, D. / STERK, M. / RANDMAA, J. | AIAA | 1980


    Flight reentry experiments

    Wilson, H. A., Jr. / Wright, R. L. | NTRS | 1964