High-pressure LOX/hydrocarbon preburner injector investigation
Author:
Affiliation:
1. Rockwell International Corp., Rocketdyne Div., Canoga Park, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-1152
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Development of a LOX/Ethanol Gas Generator for a Hybrid-Motor-Based Mini-Launcher;AIAA Propulsion and Energy 2019 Forum;2019-08-16
2. Study on Combustion Dynamic Characteristics of Oxygen-Rich Preburners;Journal of Propulsion and Power;2014-07
3. Conceptual design for a kerosene fuel-rich gas-generator of a turbopump-fed liquid rocket engine;Journal of Thermal Science;2012-09-07
4. OXIDIZER RICH PRE-BURNER FOR ADVANCED ROCKET ENGINE APPLICATION;30th Joint Propulsion Conference and Exhibit;1994-06-27
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