Gaseous Oxygen Injection Effects in Hybrid Labscale Rocket Motor Operations

Author:

Gomes Susane,Rocco Leopoldo,Rocco Jose,Iha Koshun

Publisher

American Institute of Aeronautics and Astronautics

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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