Air Force Program Office Mission Manager

Worked in the Vulcan Chief Engineer's office on successful development and integration of the launch vehicle forward systems. Responsible for system-level technical maturity of the vehicle's upper stage and interfaces, including the interstage primary structure, Centaur stage, payload fairings, ordnance, avionics, and propulsion systems.

Managed ULA's Dual Engine Centaur project, which provides a high-performance Centaur upper stage for ULA's commercial and government customers.

Designed and tested propulsion systems flight hardware for a crewed (human-rated) Atlas V mission under NASA's Commercial Crew integrated Capability (CCiCap) contract.

Developed, maintained, and innovated design solutions for the upper stage propulsion systems of the Atlas V launch vehicle, including fill/drain valves, propellant feedlines, RL10 engine components and subsystems, vent systems, and reaction control systems.- Regularly reported to and worked with external customers such as the US Air Force, NASA, DCMA, and The Aerospace Corporation- Held the role of hardware responsible engineer and technical expert for the RL10 liquid hydrogen vent system since 2009- Served as the Propulsion Systems lead design engineer for the RL10C-1 engine development program