Porous-ceramic, thermal-protection-systems are used heavily in current reentry vehicles like the Orbiter, and they are currently being proposed for the next generation of manned spacecraft, Orion. These materials insulate the structural components and sensitive electronic components of a spacecraft against the intense thermal environments of atmospheric reentry. Furthermore, these materials are also highly exposed to space environmental hazards like meteoroid and orbital debris impacts. This paper discusses recent impact testing up to 9 km/s on ceramic tiles similar to those used on the Orbiter. These tiles have a porous-batting of nominally 8 lb/cubic ft alumina-fiber-enhanced-thermal-barrier (AETB8) insulating material coated with a damage-resistant, toughened-unipiece-fibrous-insulation (TUFI) layer.


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    Titel :

    Ballistic Performance of Porous Ceramic Thermal Protection Systems at 9 km/s


    Beteiligte:
    Miller, Joshua E. (Autor:in) / Bohl, W. E. (Autor:in) / Foreman, C. D. (Autor:in) / Christiansen, Eric L. (Autor:in) / Davis, B. A. (Autor:in)

    Kongress:

    Hypervelocity Impact Symposium 2010 ; 2010 ; Freiburg, Germany


    Erscheinungsdatum :

    01.01.2009


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Ballistic Performance of Porous-Ceramic, Thermal-Protection-Systems

    Christiansen, E. L. / Davis, B. A. / Miller, J. E. et al. | NTRS | 2009


    Ballistic Performance of Porous-ceramic, Thermal Protection Systems

    Miller, J.E. / Bohl, W.E. / Christiansen, E.L. et al. | Tema Archiv | 2013


    Ceramic Based Nanomaterials for Ballistic Protection

    Magnusson, P. / Shen, Z. / North Atlantic Treaty Organization | British Library Conference Proceedings | 2006


    Thermal protection of ballistic entry vehicles

    REINIKKA, E. A. / SARTELL, R. J. | AIAA | 1965


    Ceramic composite thermal protection systems

    Fisher, R.E. / Burkland, C.V. / Bustamante, W.E. | Tema Archiv | 1985