Job Description:

Location: REMOTE

Salary: $65.00 USD Hourly - $70.00 USD Hourly

Description:

Job Summary:



Responsibilities:



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

Contact: abandyopadhyay@judge.com


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