Works in a collaborative environment, performing Missile loads and flutter /structural analysis and tests, using aeroelastic methods to solve static, time history, and frequency domain analysis Ground and flight test programs, by developing test requirements, analyzing data and documenting results Computes aeroelastic loads, by using and developing analytical models that incorporate structural, aerodynamic, and control systems characteristics and assist in performing Missile level design, fatigue and damage tolerance analyses that meet defined requirements, to support Missile level vehicle design Performs aeroelastic stability analysis, by using and developing analytical models that incorporate structural, aerodynamic, and control systems characteristics, to ensure Missile level structural stability margin requirements are met Participates in definition and verification of Missile level vehicle design meets requirements, and documents results in order to substantiate structural integrity and show compliance with customer and regulatory requirements Communicates technical approaches, results, and recommendations to engineering teams, program leadership, and customers through oral presentations and technical writing Bachelor of Science degree from an accredited course of study in engineering, mechanical, structural, civil or aerospace engineering or physics 8+ years of experience in an engineering classification or equivalent combination of education and experience 12+ years of experience in an engineering classification or equivalent combination of education and experience Masters or a PhD degree in Mechanical, Structural, Civil or Aerospace Engineering or Physics Educational or work background in aerodynamics, aeroelasticity, computational Flutter Analysis, dynamics, maneuver load analysis, structural dynamics, modern control systems and/or finite element methods Interest and experience in computational methods Experience in programming languages such as Python,