Sample Return Mission to Mars

Within this twelve person team I cooperated with another teammate on trajectory analysis, and I focused on spacecraft propulsion systems and launch vehicle specifications. I calculated the required change in velocity from Earth to Mars and back again. This allowed for the quantification of fuel and thrust needed to be attained by a combination of launch vehicles, and chemical and ion propulsion systems. Thus, I could properly size the nozzles and fuel tanks.

Commercial Supersonic Transport (SST)

This project was the design of a SST for the 2030 to 2040 time frame. I worked on engine design, which was based on material advances planned to be available during the time period. I calculated performance, thrust, fuel consumption, and designed the necessary intakes with supersonic inlets inspired by the XB-70 and SR-71. Extensively using Matlab, I formulated a flight regime that would permit a theoretical 9000 nautical mile range and Mach 2 cruise capabilities. This six person team finally presented the designs to the professor and class.