Finite Element Model development, refinement, validation, and correlation to tests
Rigid and flexible body dynamics
Modeling, simulation, and verification of spacecraft launch, docking, and landing events
Acceleration, shock, and vibration measurement and data interpretation of ground and flight tests
General loads development for spacecraft and related ground systems
Support configuration development and trade studies
Qualifications:
Minimum of a B.S. degree in mechanical, aerospace or civil engineering
5+ years of experience in the prediction/validation of low and/or high frequency structural dynamics and loads, in addition to finite element modeling
Solid foundation of structural static/dynamic fundamentals
Passion for spacecraft structural/environmental loads development/validation
Ability to solve a variety of static and dynamic structural problems using physics-based analytical methods (hand calculations, in-house tools, and 3rd party commercial analytical tools)
Ability to earn trust, maintain positive and professional relationships, and contribute to a culture of inclusion
Desired:
Spacecraft and launch vehicle loads development/validation experience
Hyperworks, NASTRAN, and Matlab proficiency
LS-Dyna proficiency
Adams proficiency
Wave6 proficiency
SEA proficiency
High frequency environment prediction skills related to spacecraft and launch vehicles
Seniority level
Mid-Senior level
Employment type
Contract
Job function
Analyst, Engineering, and Manufacturing
Industries
Defense and Space Manufacturing, Aviation and Aerospace Component Manufacturing, and Manufacturing
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