Description
The objective of this project was to design an electrically driven centrifugal pump for the Daedalus Astronautics @ASU hybrid rocket engine (HRE). The pump design was purposefully simplified due to time, fabrication, calculation, and capability constraints, which resulted in a lower fidelity design, with the option to be improved later.
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Details
Contributors
- Shillingburg, Ryan Carl (Author)
- White, Daniel (Thesis director)
- Brunacini, Lauren (Committee member)
- Mechanical and Aerospace Engineering Program (Contributor)
- Barrett, The Honors College (Contributor)
Date Created
The date the item was original created (prior to any relationship with the ASU Digital Repositories.)
2018-05
Resource Type
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