• Model-based Systems Engineering Product Owner. Led a team developing the System Architecture Model and system requirements for the GWS (GMD Weapon System) program• Manual Test Team lead. Managed a team of over 10 people to author and execute test cases. Led the effort to change from testing at the end of the release to continuously testing during each sprint• GMD Launch Manager Product Owner. Managed a team of over 30 people responsible for planning and executing an entire release worth of work for the most complicated product within Launch Support Systems. Led the team through a time of rapid and intense change while still meeting commitments.• Lead systems engineer responsible for implementing automated testing capability• GMD Launch scrum master

• Led all aspects of design and coordination of parabolic test flight for the Human Landing System, including supplier management, cost, schedule, and technical content of test planning and execution

• Led development of cohesive, insightful domain and technology plans to ensure enterprisealignment of technology strategy and investment, and presented to CTO leadership team• Orchestrated enterprise summits to improve understanding of antenna capabilities, leadingto identification of leveraging opportunities across business units

• Responsible for creating the vision and driving the execution of multiple teams to produce contractual deliverables, interface with government customer, and drive program-wide process improvements, resulting in substantial cost savings and time savings, and high customer satisfaction• Implemented new program process to clearly delineate differences between risks, issues, and limitations, to prevent duplication of work and increase role clarity across groups• Identified and implemented multiple improvements to internal team process and database, reducing time and rework required to generate reports• Provided technical leadership, mentorship and development for early and mid-career systems engineers• Leveraged knowledge of the whole company to bring “best of enterprise” solutions to program-specific problems

• Performed systems engineering and design integration for the Space Launch System (SLS) Core Stage (CS) and Exploration Upper Stage (EUS), Block 1 and Block 1B. Successfully coordinated between multiple product teams and stakeholders, emphasizing first-time quality and meeting aggressive program schedule milestones• Served as a primary integrator for wide variety of systems, including ground interfaces, reaction control system, flight pressurization, thrust vector control, and purge, vent and hazardous gas detection. Also supported main propulsion system, primary structures, and engine integration• Designed an integration tool which has become integral to the EUS design process, resulting in over $1.2M in cost avoidance and received an SLS Innovation Award• Provided technical mentorship and development for early career systems engineers

• Developed over 1,500 failure modes and effects analyses (FMEAs) for the flight termination, thermal protection, power distribution, structures, umbilical, and purge, vent and hazardous gas subsystems for the Space Launch System• Responsible for revision and release of the Limited Life Item document• Spearheaded change which resulted in significant cost and schedule savings by eliminating the need for several hundred FMEAs• Recognized for going above and beyond to impress the customer (NASA) by presenting important issues and volunteering to take responsibility for additional subsystems to help the group meet deadlines

• Developed repairs for the fuselage for the 737-NG and 757 Structural Repair Manuals (SRMs) responsible for eliminating 110 Service Requests per year• Received 2011 Commercial Aviation Services (CAS) Service Excellence award for reducing flowtime for developing SRM procedures by ~66%• Main developer of electronic data solution for delivering structural engineering data to customers• Authored 16 of the 19 repairs released in the SRM in 2011 for the 737-900ER• Work Statement Requirements Database (WSRD) Focal for the SRM group

• Conducted research for the Horizontal Launch Study for SST0 and TSTO launch vehicles, ablative materials for TPS, metal matrix composites, and interplanetary trajectory calculations