- Team lead on the development and construction of a test stand for a liquid oxygen and isopropyl rocket engine- Design of piping system, creation of Piping and Instrumentation Diagrams, and parts selection for high pressure and cyrogenic fluids- Testing and redesign of multiple critical systems including pintle type injector for 500 lb force rocket motor and main propellant valves- Created parametric CFD models of pintle type injector enabling rapid changes to critical flow geometry- Used CFD simulations to improve injector design and to meet engine mass flow rate requirements

Summer internship with the Satellite Servicing Projects Division at GSFC. - Assembly, integration and testing of spaceflight hardware and mechanisms for the Robotic Refueling Mission 3 Tool Pedestal, mission launched to ISS on December 5, 2018 - Performed venting analysis for Robotic Tool Stowage mission, determined required number and size of venting holes and met critical design review requirement - Worked with NASA engineers on thermal, functional, life cycle, and vibration testing of Tool Pedestal, compiled results of thermal / functional testing into final report. - Designed fixture for impact testing of light diffusing material which is to be used on a robotic tool stowage mission to the International Space Station