AERO 653 Space Propulsion
The course focuses on rocket propulsion systems, their physics, their performance, their sizing and their mission design. Students are exposed to ideal rocket propulsion system performance prediction as well as the effects associated with deviations from ideal behavior. Propulsion system design is emphasized with a discussion on mission requirements, and launch analysis is included to enable complete sizing studies. The course provides an understanding of the thermo-fluid dynamic concepts underlying rocket space propulsion and their implications for launch vehicle and spacecraft system performance and design. Combustion and thermochemistry provide the theoretical foundations to understand chemical engines. Basics of electrical and electromagnetic thrusters are also taught.