Description
Derived from the necessity to increase testing capabilities of hybrid rocket motor (HRM) propulsion systems for Daedalus Astronautics at Arizona State University, a small-scale motor and test stand were designed and developed to characterize all components of the system.
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Contributors
- Summers, Matt H (Author)
- Lee, Taewoo (Thesis advisor)
- Chen, Kangping (Committee member)
- Wells, Valana (Committee member)
- Arizona State University (Publisher)
Date Created
The date the item was original created (prior to any relationship with the ASU Digital Repositories.)
2013
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Note
- Partial requirement for: M.S., Arizona State University, 2013Note typethesis
- Includes bibliographical references (p. 85-86)Note typebibliography
- Field of study: Aerospace engineering
Citation and reuse
Statement of Responsibility
by Matt H. Summers