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Improved performance parameter always important in any propulsion system. Various methods has been used for this improvement. In the present study, disturbing the flow of oxidizer using protrusion has been tried. It improves regression rate or burn rate along with combustion efficiency of hybrid rocket.

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This page is a summary of: Utility of Multiprotrusion as the Performance Enhancer in Hybrid Rocket Motor, Journal of Propulsion and Power, September 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37491.
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