Tell a friend
Print
H2/O2 Rocket Combustor Flow Field Modeling, Simulation and Analysis.
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.
Full text not available from this repository.
| 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: |
| ||||||
| Date: | 1997 | ||||||
| Journal or Publication Title: | 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle, WA, July 7-9, 1997 | ||||||
| Series Name: | AIAA 97-3300 | ||||||
| Status: | Published | ||||||
| Keywords: | H2/O2, Rocket Combustor, Rocket engine, | ||||||
| HGF - Research field: | UNSPECIFIED | ||||||
| HGF - Program: | Space | ||||||
| HGF - Program Themes: | W RP - Raumtransport | ||||||
| DLR - Research area: | UNSPECIFIED | ||||||
| DLR - Program: | W RP - Raumtransport | ||||||
| DLR - Research theme (Project): | E -- no assignement | ||||||
| Location: | Lampoldshausen | ||||||
| Institutes and Institutions: | Institute of Space Propulsion | ||||||
| Deposited By: | elib DLR-Beauftragter | ||||||
| Deposited On: | 02 Apr 2006 | ||||||
| Last Modified: | 27 Apr 2009 05:42 |
Repository Staff Only: item control page
