Date of Award:
Master of Science (MS)
Mechanical and Aerospace Engineering
Hybrid rockets are rockets which employ a solid fuel grain with a liquid oxidizer. Hybrids have many promising potential applications, however they also have a few drawbacks. Of interest to this research is the increased rate of nozzle erosion inherent to hybrid rockets. In order to address this issue, a low-erosion nozzle is proposed and evaluated.
Stephens, Judson C., "Development of an Anisotropic Thermal Stress Model for a Low-Erosion Hybrid Rocket Nozzle System" (2021). All Graduate Theses and Dissertations. 8198.
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