• Led design, assembly, and testing from concept ideation to completion of opto-mechanical shutter mechanism on Raytheon’s first commercial satellite program
• Designed and modeled >60 3D CAD parts informed by FEA, DFM, DFA
• Created and toleranced part and assembly drawings with high-precision GD&T, releasing in a PDM system
• Collaborated with SMEs, Engineers (Optical, Structural/Thermal Analysis, System, Test), Supply Chain, etc.
• Inspected vendor deliverables at supplier location; managed delivery dates, nonconformances
• Prototyped, developed, and implemented new magnetic damper system to meet strict space material constraints
• Built and tested multiple mechanisms in record time with zero failures, working under tight commercial deadlines
Responsible Engineering Authority leading design, manufacture, assembly, and testing of an opto-mechanical space mechanism for use in a fast-paced, high-volume commercial satellite program.
In this role, I was leading the mechanism's development for the entire product life cycle from concept to sell-off to the larger payload. This involved creating the 3D CAD models, 2D CAD drawings, test/assembly equipment design, working with suppliers, writing assembly instructions and test plans/procedures, assembling the hardware, testing the hardware, and integrating it into the next higher assembly. Resulting from these efforts were several space-qualified mechanisms that were built and tested in record time for a space mechanism.
Since then, my mechanical engineering and product life cycle expertise has been utilized on other space programs, from proposal programs to other multi-payload opto-mechanical satellite programs.