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Closed-Loop Thrust and Pressure Profile Throttling of a Nitrous Oxide/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor

Degree

thesis:*
Name thesis:degree_name
Master of Science (MS)
Level thesis:degree_level
Thesis
Grantor dc:publisher
Hosted by Utah State University Libraries

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Peterson, Zachary W.
Contributors dc:contributor
  • Stephen A. Whitmore
  • R. Rees Fullmer
  • David K. Geller

Subjects

dc:subject × 9

Identifiers

dc:identifier.*
Repository record dc:identifier
https://digitalcommons.usu.edu/etd/1400
OAI identifier oai:identifier
oai:digitalcommons.usu.edu:etd-2407

Chain of custody

source
Harvested from
Utah State University
Base URL
digitalcommons.usu.edu/do/oai/
Last updated
2026-07-27
Source record
OAI-PMH GetRecord
citation

Peterson, Zachary W.. Closed-Loop Thrust and Pressure Profile Throttling of a Nitrous Oxide/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor. Thesis thesis, Hosted by Utah State University Libraries, https://digitalcommons.usu.edu/etd/1400