Hybrid Rocket Engine Design Utilizing a Polymer Matrix Encapsulating Pulverized Fuel

Author

Seth Holladay, University of Tennessee, KnoxvilleFollow
Teague Aarant, University of Tennessee, KnoxvilleFollow
Jared Bass, University of Tennessee, KnoxvilleFollow
Timothy Grizzel, University of Tennessee, KnoxvilleFollow
Matthew McVey, University of Tennessee, KnoxvilleFollow
William Putthoff, University of Tennessee, KnoxvilleFollow
Angus Shaw, University of Tennessee, KnoxvilleFollow
Caroline Littel, University of Tennessee, KnoxvilleFollow
James Evans Lyne, University of Tennessee, KnoxvilleFollow

Date of Graduation

5-2019

College

Aerospace Engineering

First Advisor

Dr. James Evans Lyne

Recommended Citation

Holladay, Seth; Aarant, Teague; Bass, Jared; Grizzel, Timothy; McVey, Matthew; Putthoff, William; Shaw, Angus; Littel, Caroline; and Lyne, James Evans, "Hybrid Rocket Engine Design Utilizing a Polymer Matrix Encapsulating Pulverized Fuel" (2019). Chancellor’s Honors Program Projects.
https://trace.tennessee.edu/utk_chanhonoproj/2273