Eggers, T. (2004) Aerodynamic and Aerothermodynamic Layout of the Hypersonic Flight Experiment SHEFEX. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln (de), 08.-11.11.2004.
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The purpose of the SHarp Edge Flight EXperiment SHEFEX is the investigation of possible new shapes for future launcher or reentry vehicles . The main focus is the improvement of common space vehicles shapes by application of facetted surfaces and sharp edges. The experiment will enable the time accurate investigation of the flow effects and their structural answer during the hypersonic flight from 90 km down to an altitude of 20 km. The project, being performed under responsibility of the German Aerospace Center (DLR) is scheduled to fly on top of a two-stage solid propellant sounding rocket for the first half of 2005. The paper contains a survey of the aerodynamic and aerothermodynamic layout of the experimental vehicle. The results are inputs for the definition of the structural layout, the TPS and the flight instrumentation as well as for the preparation of the flight test performed by the Mobile Rocket Base of DLR.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Aerodynamic and Aerothermodynamic Layout of the Hypersonic Flight Experiment SHEFEX|
|Keywords:||Hypersonic aerodynamics, aerothermodynamics, flight experiment, future launcher|
|Event Title:||5th European Symposium on Aerothermodynamics for Space Vehicles, Köln (de), 08.-11.11.2004|
|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 19:47|
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