Weiland, C. and Longo, J.M.A. and Gülhan, A. and Decker, K. (2002) Aerothermodynamics for Reusable Launch Systems. Deutscher Luft- und Raumfahrtkongress 2002, Stuttgart (de), 23.-26.09.2002.
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The development of modern spacecrafts (launch and re-entry vehicles), either fully reusable or partly reusable needs powerful tools for the design of the aerodynamic shape with a guarantee for reliable flight and controllability along the complete ascent and descent trajectories. Experimental and numerical tools are available these days and for improving the reliability of vehicle design their capability has to be improved step by step. In the frame of the German TETRA Program very in detail technology work was carried out to reach this goal. The growth of the efficiency of these methods is demonstrated by some specific aerothermodynamic problems about which are reported in this paper.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=2003, monograph_id=DGLR-paper 2002-152,|
|Title:||Aerothermodynamics for Reusable Launch Systems|
|Keywords:||Aerothermodynamics, Wind Tunnel Test, CFD, Real Gas, RCS|
|Event Title:||Deutscher Luft- und Raumfahrtkongress 2002, Stuttgart (de), 23.-26.09.2002|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Space (old)|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||Space|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||Claudia Grant|
|Deposited On:||31 Jan 2006|
|Last Modified:||14 Jan 2010 19:06|
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