eTD Explore

Start Over Degree MS Keyword CubeSat Keyword regression rate Author Last Name Mcknight

1. Advanced Hybrid Rocket Motor Propulsion Unit For CubeSats

open_access

Open Access

Author:: Mcknight, Brendan Robert
Title:: Advanced Hybrid Rocket Motor Propulsion Unit For CubeSats
Graduate Program:: Mechanical Engineering
Keywords:: additive manufacturing
CubeSat
hybrid rocket motor
regression rate
combustion efficiency
File:: Download 1-McKnight_Thesis.pdf
Committee Members:: Richard A Yetter, Thesis Advisor/Co-Advisor