At the Space Launcher System Analysis (SART) department of DLR-Cologne, a hypersonic spaceplane for passenger transportation is being investigated. The spaceplane is called the “SpaceLiner”. The vehicle performs its rocket powered, intercontinental flight via a suborbital trajectory. The major challenge is the aerodynamic heating of the vehicle. This is discussed, and a possible solution for handling the extreme heatloads will be presented. The solution involves an innovative new way of transpiration cooling, using liquid water.


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    Titel :

    Transpiration Cooling Methods for the SpaceLiner


    Beteiligte:
    Gülhan, Ali (Herausgeber:in) / van Foreest, A. (Autor:in) / Sippel, M. (Autor:in) / Gülhan, A. (Autor:in) / Esser, B. (Autor:in)


    Erscheinungsdatum :

    2008-01-01


    Format / Umfang :

    16 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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