The SH arp E dge F light EX periment (SHEFEX) of the German Aerospace Center (DLR) has been established to demonstrate the feasibility of space vehicles with facetted Thermal Protection System (TPS). In this study, first results to the aerothermodynamic behavior of SHEFEX-II in the High Enthalpy Shock Tunnel Göttingen (HEG) are presented.The main focus is on the experimental and numerical investigation of the active cooling experiment AKTiV . The measured and calculated results confirm that a cooling effect is feasible.


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    Titel :

    Experimental and Numerical Analysis of SHEFEX-II


    Beteiligte:
    Barth, Tarik (Autor:in) / Gehre, Rolf (Autor:in) / Eggers, Thino (Autor:in) / Schramm, Jan Martinez (Autor:in) / Wagner, Alexander (Autor:in) / Hannemann, Klaus (Autor:in) / Kaufmann, Rene (Autor:in) / Böhrk, Hannah (Autor:in)


    Erscheinungsdatum :

    2013


    Format / Umfang :

    9 Seiten





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Advanced aerothermodynamic analysis of SHEFEX I

    Barth, Tarik | Online Contents | 2010


    Advanced Flight Analysis of SHEFEX-I

    Barth, Tarik / Longo, Jose M. | Tema Archiv | 2010


    The Flight of SHEFEX

    Püttmann, Norbert / Longo, Dr. José | AIAA | 2006


    Flight Control of SHEFEX II

    Scheuerpflug, F. / Kallenbach, A. / European Space Agency | British Library Conference Proceedings | 2013


    The Hypersonic Flight Experiment SHEFEX

    Eggers, Thino / Longo, Jose / Hoerschgen, Marcus et al. | AIAA | 2005