MG 486 Rocket & Spacecraft Propulsion

This course entails the study of rocket and spacecraft propulsion systems ranging from monopropellant thrusters, solid propellant rocket motors (SRMs) to the latest high performance Methane-LOX engines used on the SpaceX Starship. Attention will focus on the design, operation, and performance differences and the evolution of rocket engines since the early 1900s. Students will learn the advantages and disadvantages of the various engine types and how these parameters govern their application to specific mission types and performance regimes. Elementary performance calculations will be presented and contrasted. A life-cycle cost approach will be employed to include development, fixed, and variable operating costs and performance. Overall operations and maintenance of engines will likewise be addressed. A systems management light will be cast on the subject to include fixed and variable operating costs, performance, reliability, and maintenance. Potential future systems such as ion, nuclear, and even warp drive propulsion systems will also be addressed.

Credits

3