Barth, Tarik (2010) Aerothermodynamische Untersuchung facettierter Raumfahrzeuge unter Wiedereintrittsbedingungen. Dissertation, Universität Stuttgart.
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Official URL: http://elib.uni-stuttgart.de/opus/volltexte/2010/5652/
| Item URL in elib: | https://elib.dlr.de/65646/ | ||||||||
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| Document Type: | Thesis (Dissertation) | ||||||||
| Title: | Aerothermodynamische Untersuchung facettierter Raumfahrzeuge unter Wiedereintrittsbedingungen | ||||||||
| Authors: |
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| Date: | September 2010 | ||||||||
| Refereed publication: | Yes | ||||||||
| Open Access: | Yes | ||||||||
| Number of Pages: | 147 | ||||||||
| Status: | Published | ||||||||
| Keywords: | SHEFEX, facettiertes Thermalschutzsystem, Freiflugexperiment, Wiedereintritt, gekoppelte Simulation, | ||||||||
| Institution: | Universität Stuttgart | ||||||||
| 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 - Raumfahrzeugsysteme - Rückkehrtechnologie (old), W - Grundlagen Raumtransport - numerische Verfahren (old), W - Rückkehrtechnologie - Innovativer Thermalschutz (old), W - Raumfahrzeugsysteme - Numerische Verfahren und Simulation (old), W - Grundlagen Raumtransport - Innovativer Thermalschutz (old), W - Grundlagen Raumtransport - Anlagen und Messtechnik (old), W - SHEFEX Programm (old) | ||||||||
| Location: | Stuttgart , Braunschweig , Göttingen | ||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Spacecraft Institute of Structures and Design > Space Structural Components | ||||||||
| Deposited By: | Barth, Tarik | ||||||||
| Deposited On: | 18 Oct 2010 10:40 | ||||||||
| Last Modified: | 31 Jul 2019 19:28 |
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