LOX-Kerosene Oxidizer-Rich Gas-Generator and Main Combustion Chamber Subscale Testing
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Publisher
American Institute of Aeronautics and Astronautics
Reference3 articles.
1. Preclik, D., Hagemann, G., Knab, O., Brummer, L., Mäding, C., Wiedmann, D. "LOX-Hydrocarbon Propellant Trade Considerations for Future Reusable Liquid Booster Engines," AIAA-2005-3567, 41st AIAA/ASME/SAE/ASEE Joint Propulsion ConferenceandExhibit,Tucson, Arizona, 10-13July2005.
2. Haeseler, D., Mäding, C., Götz, A., Rubinski, V., Khrissanfov, S., Berejnoy, V. "Testing of LOX-Hydrocarbon Thrust Chambers For Future Reusable Launch Vehicles," AIAA-2002-3845, 38th AIAA/ASME/SAE/ASEE Joint Propulsion ConferenceandExhibit, Indianapolis, Indiana, 7-10July2002.
3. Non-toxic propellants for future advanced launcher propulsion systems
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