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
Included in
Copyright for this work is retained by the student. If you have any questions regarding the inclusion of this work in the Digital Commons, please email us at DigitalCommons@usu.edu.
