Structural Analyst
Current-Developed PATRAN/NASTRAN finite element models (FEM) to perform static (inertial loads, thermal stress) and dynamic (random vibration and modal analyses) analyses for various satellite payload piece parts, assemblies, and test equipment; post processed stress and bolt force results to provide suggestions for improvement of material margins and optimizization of design-Designed and conducted case study to characterize vibrations from helium compressors on thermal vacuum chamber structure to reduce noise on the unit under test inertial measurement unit data -Responsible engineer for various environmental tests such as random vibration and mechanical alignment; verified test setup, inputs and results for various payload assemblies to validate design