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)
Acceleration, shock, and vibration measurement and data interpretation of ground and flight tests
Modeling, simulation, and verification of spacecraft launch, in-space burns, and landing events
Finite Element Model development, refinement, validation, and correlation to tests
General loads development for spacecraft and related ground systems
Support configuration development and trade studies
Requirements
Minimum of a B.S. degree in mechanical, aerospace or civil engineering
3+ 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)
Benefits
Medical, dental, vision, basic and supplemental life insurance
Paid parental leave
Short and long-term disability
401(k) with a company match of up to 5%
Education Support Program
Stock Options for all regular employees (working at least 20 hours/week)
Paid Time Off: Up to four (4) weeks per year based on weekly scheduled hours