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Schweitzer, C. and Schley, C.-A. (1997) H2/O2 Rocket Combustor Flow Field Modeling, Simulation and Analysis. In: 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle, WA, July 7-9, 1997.
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| Item URL in elib: | https://elib.dlr.de/25088/ | |||||||||
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| Document Type: | Conference or Workshop Item (Paper) | |||||||||
| Additional Information: | LIDO-Berichtsjahr=1997, pages=20, | |||||||||
| Title: | H2/O2 Rocket Combustor Flow Field Modeling, Simulation and Analysis. | |||||||||
| Authors: |
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| Date: | 1997 | |||||||||
| Journal or Publication Title: | 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle, WA, July 7-9, 1997 | |||||||||
| Open Access: | No | |||||||||
| Gold Open Access: | No | |||||||||
| In SCOPUS: | No | |||||||||
| In ISI Web of Science: | No | |||||||||
| Series Name: | AIAA 97-3300 | |||||||||
| Status: | Published | |||||||||
| Keywords: | H2/O2, Rocket Combustor, Rocket engine, | |||||||||
| HGF - Research field: | UNSPECIFIED | |||||||||
| HGF - Program: | Space (old) | |||||||||
| HGF - Program Themes: | W RP - Raumtransport | |||||||||
| DLR - Research area: | UNSPECIFIED | |||||||||
| DLR - Program: | W RP - Raumtransport | |||||||||
| DLR - Research theme (Project): | E - no assignment | |||||||||
| Location: | Lampoldshausen | |||||||||
| Institutes and Institutions: | Institute of Space Propulsion | |||||||||
| Deposited By: | DLR-Beauftragter, elib | |||||||||
| Deposited On: | 02 Apr 2006 | |||||||||
| Last Modified: | 27 Apr 2009 05:42 |
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