College - Author 1
College of Engineering
Department - Author 1
Aerospace Engineering Department
Degree Name - Author 1
BS in Aerospace Engineering
Date
2-2013
Primary Advisor
Daniel Wait, College of Engineering, Aerospace Engineering Department
Abstract/Summary
The Static Methanol Oxygen Rocket Engine (SMORE) has undergone several revisions since its inception. This latest revision aimed to increase startup reliability and user safety in the operation of the rocket. The implementation of maintenance procedures, safeguards in the ignition system, as well as construction of a new control box and redesign of the igniter itself have accomplished these goals while keeping costs down and without modifying the current rocket setup. Startup reliability has increased drastically, so long as all other rocket setup procedures are followed properly. 250 subsequent firings of the rocket have proven an igniter reliability of more than 90%. All parts replaced and manufactured in this report have been well documented to ensure ease of maintenance in the future.
URL: https://digitalcommons.calpoly.edu/aerosp/105
Included in
Propulsion and Power Commons, Systems Engineering and Multidisciplinary Design Optimization Commons