Gaseous Oxygen Injection Effects in Hybrid Labscale Rocket Motor Operations
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Publisher
American Institute of Aeronautics and Astronautics
Reference5 articles.
1. Studies on a Pressurized Swirl Injector Bi-Propellant Used in Rocket-Motor
Cited by 5 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. Design and Testing of a Lab-Scale Hybrid Rocket Motor to Evaluate Swirl Injection Characteristics;Energetic Materials Research, Applications, and New Technologies;2018
2. Combustion evaluation of PU solid fuel based on pre-polymer technology additivated with paraffin and Aluminum for hybrid rocket engines;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30
3. Evaluation of polyurethane binder additivated with paraffin and tested with a swirl injector;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30
4. The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30
5. Design and Testing of a Hybrid Rocket Motor;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31
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