Date

2-2013

Degree Name

BS in Aerospace Engineering

Department

Aerospace Engineering Department

Advisor(s)

Dan Wait

Abstract

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.