FURI | Spring 2019

Propellant Mixing in Vortex Cooled Liquid Rocket Engines

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As temperatures in the combustion chamber of a liquid rocket engine during use can exceed 5,000 °F, a large portion of development is often focused on cooling. However, by injecting propellants tangential to the combustion chamber it is possible to create a vortex which separates hot combustion gases from the chamber wall. By studying this mechanism, cooling system complexity can be reduced while increasing engine efficiency.

Student researcher

James Hansen

James Hansen

Aerospace engineering

Hometown: Glendale, Arizona

Graduation date: Spring 2021

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