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Aerothermodynamische Untersuchung facettierter Raumfahrzeuge unter Wiedereintrittsbedingungen

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/


Document Type:Thesis (Dissertation)
Title:Aerothermodynamische Untersuchung facettierter Raumfahrzeuge unter Wiedereintrittsbedingungen
Authors:
AuthorsInstitution or Email of Authors
Barth, TarikTarik.Barth@dlr.de
Date:September 2010
Refereed publication: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), Aeronautics, Space and Transport (old), Aeronautics, Space and Transport (old), Aeronautics, Space and Transport (old), Aeronautics, Space and Transport (old), Aeronautics, Space and Transport (old), Aeronautics, Space and Transport (old)
HGF - Program:Space (old), Space (old), Space (old), Space (old), Space (old), Space (old), Space (old)
HGF - Program Themes:W RP - Raumtransport, W RP - Raumtransport, W RP - Raumtransport, W RP - Raumtransport, W RP - Raumtransport, W RP - Raumtransport, W RP - Raumtransport
DLR - Research area:Space, Space, Space, Space, Space, Space, Space
DLR - Program:W RP - Raumtransport, W RP - Raumtransport, W RP - Raumtransport, W RP - Raumtransport, W RP - Raumtransport, W RP - Raumtransport, 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: Tarik Barth
Deposited On:18 Oct 2010 10:40
Last Modified:09 Apr 2013 10:43

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