Labbe, S.G. and Perez, L.F. and Fitzgerald, S. and Longo, J.M.A. and Rapuc, M. (1999) X-38 NASA/DLR/ESA-Dassault Aviation Integrated Aerodynamic and Aerothermodynamic Activities. Int. Symposium Atmospheric Reentry Vehicles and Systems, Arcachon (fr), 16.-18.03.1999.
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The characterization of the aeroshape selected for the X-38 (Crew Return Vehicle (CRV) demonstrator) is presently being performed as a cooperative endeavour between NASA, DLR (through its TETRA Program), and the European Space Agency (ESA) with Dassault Aviation integrating the aerodynamic and aerothermodynamic activities. The methodologies selected for characterizing the aerodynamic and aerothermodynamic environment of the X-38 are presented. Also, the implications for related disciplines such as Guidance Navigation and Control (GN&C) with its corresponding Flight Control System (FCS), Structural, and Thermal Protection System (TPS) design are discussed. An attempt is made at defining the additional activities required to support the design of a derived operational CRV.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||X-38 NASA/DLR/ESA-Dassault Aviation Integrated Aerodynamic and Aerothermodynamic Activities|
|Keywords:||Lifting Body, Aerodynamic, Aerothermodynamic, Vehicle Design|
|Event Title:||Int. Symposium Atmospheric Reentry Vehicles and Systems, Arcachon (fr), 16.-18.03.1999|
|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 > Institut für Entwurfsaerodynamik|
|Deposited By:||Claudia Grant|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 20:02|
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