What is it about?
In this study, a novel injector concept is proposed for advanced hybrid rockets which provides very high fuel regression rate when compared motors with classical injector configuration. 30 motor firings were performed and non-dimensional scaling rule was developed with high accuracy for this injector concept.
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This page is a summary of: Regression Rate Enhancement of Hybrid Rockets by Introducing Novel Distributed Tube Injector, Journal of Propulsion and Power, March 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b38417.
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