Co-led effort to redesign stronger and lighter load bearing brackets using mathematical modeling programs

Verified that new bracket designs meet safety regulations without incurring additional manufacturing costs

Spearheaded cost-reduction objectives in the CCTS design leading to $25K (10% of total design cost) in savings

Incorporating panel defects into mathematical model to ensure test panels are still valid for testing on SLS

Supported structural analysis on press and feedlines to help suppliers meet NASA design requirements

Simulated barrel panel forming resulting in roughly $200,000 saved in manufacturing and testing costs