B.S. degree in mechanical, aerospace engineering, or a comparable field 8+ years of experience performing L&D analysis Comfortable working in a fast-paced, startup environment Expertise in dynamic analysis methods (structural dynamics, dynamic loads, acoustics, modal, random vibration, shock response) Working experience in loads development for vehicle and/or engine applications Experience anchoring analytical models to physical testing M.S. degree or higher in Mechanical, Aerospace Engineering, or a comparable field, ideally focusing on solid mechanics, fatigue, fracture, or structural dynamics Experience with flutter analysis GFEM development and model grounding experience Knowledge of turbomachinery-related analytical methods High Cycle Fatigue Analysis (HCF) Low Cycle Fatigue Analysis (LCF) Experience performing Finite Element Analysis (FEA / FEM) using commercial codes (e.g., ANSYS, Abaqus, or NASTRAN-based solvers) Experience with Femap/Nastran Fracture analysis (crack growth / safe-life and assessing for instability via LEFM, ideally with prior experience using NASGRO) Experience with the ANSYS FEA suite A strong theoretical background in heat transfer, fluid mechanics, and/or compressible flow Prior experience working on safety-critical systems in production environments Prior professional experience working on either rocketry or turbomachinery Experience supporting failure investigations and root-cause analysis A track record of working efficiently in fast-paced engineering environments A track record of effective oral and written communications to support your recommendations Thermal-Structural static analysis Fluid analysis (e.g. Computational Fluid Dynamics / CFD or 1-D transient analysis using SINDA/FLUINT or ROCETS) Knowledge of composite materials, insulation, and ablative thermal protection systems