- Conducted schedule risk assessments by leveraging existing customer provided data andhistorical data comparisons.- Performed Monte Carlo statistical analysis to determine programmatic risk using internalsoftware tools, and subject matter experts for risk distributions.- Designed satellite propulsion system for customer programs within the Concept DevelopmentCenter (CDC).- Created cost estimation for program development, production, and mission lifecycle based oninternally developed software tools and historical data.- Work completed lead to revisions in customer program timelines, and satellite configurations.

- Responsible for all research and development of aerodynamic elements, and aerodynamic analysis.- Created and presented preliminary and critical design review reports to advisors and industry. - Reduced nose cone mass by 60% using lightweight carbon fiber composites.- Implemented agile manufacturing processes with additive manufacturing, and 3D printing.- Optimized vehicle performance using CFD and FEA.- Designed external ignition system and carbon fiber composite boat tail.- Performed aerodynamic analysis using SolidWorks Flosim, FinSim, OpenRocket, and RasAero 2.

-Responsible for assembling, operating, and trouble shooting all mechanical support equipment during static fires, and launch vehicle tests. - Lead team in assembling and orienting launch rail in accordance to procedures.- Facilitate launch vehicle mounting and pre-test ground equipment safety checks.

- Assist in the design, fabrication, and integration of aerodynamics components.- Perform research and design of thermal protection system for atmospheric reentry.- CFD analysis using Solidworks FloSim, OpenRocket, and OpenFoam.

- Fabricated fiberglass composites body tubes through wet layups. - Fabricated silica phenolic thrust chambers.- Fabricated carbon fiber composite plates for use in composite rocket fins.