Date of Award
2015
Document Type
Thesis
Degree Name
Master of Science in Engineering (MSE)
Department
Mechanical and Aerospace Engineering
Subject(s)
Hybrid propellant rockets., Rocket engines--Combustion.
Recommended Citation
Mascaro, Michael D., "Regression rate determination of a gas generator hybrid rocket motor with GOX" (2015). Theses. 151.
https://louis.uah.edu/uah-theses/151
COinS