Title: Design of a Novel Gaseous Hydrogen-Oxygen Rocket Injector Element
Abstract: An overview of activities supporting the design of a gaseous hydrogen-oxygen rocket injector element is presented in viewgraph form. The purpose of the research was to find a viable design for a rocket gas-gas injector that mixes fuel and oxidizer thoroughly and quickly. Computational fluid dynamics analyses were used with reacting flow to evaluate design options for mixing, temperature distribution, and combustion efficiency. A design was found that is an improvement over designs derived from liquid systems and is far better than traditional shear-coax.
Publication Year: 1999
Publication Date: 1999-01-01
Language: en
Type: article
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