Kühlwein, Georg (2012) Auslegung und Konstruktion einer Hochdruck-Raketenschubkammer für die Treibstoffkombination Wasserstoff/Sauerstoff. DLR-Interner Bericht. DLR-IB 647-2012/4. Diploma. Universität Stuttgart, Germany.
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Item URL in elib: | https://elib.dlr.de/78377/ | ||||||||
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Document Type: | Monograph (DLR-Interner Bericht, Diploma) | ||||||||
Title: | Auslegung und Konstruktion einer Hochdruck-Raketenschubkammer für die Treibstoffkombination Wasserstoff/Sauerstoff | ||||||||
Authors: |
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Date: | 2012 | ||||||||
Open Access: | No | ||||||||
Status: | Published | ||||||||
Keywords: | Raketenbrennkammer, H2, O2 | ||||||||
Institution: | Universität Stuttgart, Germany | ||||||||
Department: | Institut für Raumfahrtsysteme | ||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||
HGF - Program: | Space | ||||||||
HGF - Program Themes: | Space Transportation | ||||||||
DLR - Research area: | Raumfahrt | ||||||||
DLR - Program: | R RP - Space Transportation | ||||||||
DLR - Research theme (Project): | R - Antriebsystemtechnik - Schubkammertechnologie (old) | ||||||||
Location: | Lampoldshausen | ||||||||
Institutes and Institutions: | Institute of Space Propulsion > Rocket Propulsion | ||||||||
Deposited By: | Hanke, Michaela | ||||||||
Deposited On: | 12 Nov 2012 10:34 | ||||||||
Last Modified: | 01 Dec 2018 19:48 |
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