RAPHAEL AUBRY; GINES RODRIGUEZ CASTRO; ELOUAN MAITRE; ANGELIKI PARISI PLOUMPI; JACOB AMALER

DOI Number: 10.13009/EUCASS2023-036

The objective of this work is to develop a sizing tool for impinging and coaxial-type injectors. The tool is built on a database of experimental and theoretical correlations available in the literature for the design of liquid rocket engine injectors. They relate the injector element geometries and propellant properties to the injection pressure losses, liquid droplet size and mixing performance. Doublet impinging, swirl coaxial and shear coaxial element geometries were sized using the tool and presented with their expected respective performances. It is the aim of this work to be a building block for the design of injectors within the PERSEUS project.

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In Categories: 1. Aerospace Europe Conference 2023, 1.Events, 13. Space Student Programs
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