Date of Award:
8-2021
Document Type:
Thesis
Degree Name:
Master of Science (MS)
Department:
Mechanical and Aerospace Engineering
Committee Chair(s)
Stephen Whitmore
Committee
Stephen Whitmore
Committee
David Geller
Committee
Randy Christensen
Abstract
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.
Checksum
985b990feebb5822d913fde6e50c71df
Recommended Citation
Stephens, Judson C., "Development of an Anisotropic Thermal Stress Model for a Low-Erosion Hybrid Rocket Nozzle System" (2021). All Graduate Theses and Dissertations, Spring 1920 to Summer 2023. 8198.
https://digitalcommons.usu.edu/etd/8198
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