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Key job responsibilities
- Perform structural/dynamic loads analyses, and multi-body dynamic simulations for subsystem and vehicle level trades.
- Contribute to spacecraft structural/dynamics test planning, equipment and instrumentation selection, and data acquisition.
- Create & maintain FEA models for all vehicle states: GSE/transport, launch vehicle (stowed), on-orbit states (dispensing, deployments).
- Pretest simulations, response limiting/notching definition, and post-test data analysis and correlation/validation of analytical model.- Pointing accuracy trades; build dynamic disturbance models from spacecraft MMAs, and incorporating predictions of thermal profile transients, to identify and mitigate jitter effects on pointing precision.Export Control Requirement:
A day in the lifeRedmond, WA, USA
- 6+ years of working in mechanical engineering or equivalent experience
- 3+ years of experience in dynamic analysis and testing (modal, random vibration, shock, and/or acoustics)
- 3+ years experience with finite element analysis NASTRAN (or equivalent)
- 5+ years of experience with model preparation delivery and interpretation of results for coupled load analysis, including experience with component modal synthesis reduction techniques, such as Craig-Bampton;
- 5+ years of experience in on orbit disturbance modeling and multi-body dynamics;
- 5+ years of experience with modal testing and correlation of hardware
- Masters in mechanical engineering, aerospace engineering, or related field;
- Demonstrated experience in several of the following areas:
- Experience with full vehicle qualification for flight;
- Experience testing components and vehicles.
- Dynamics analysis with MSC ADAMS, LS-Dyna, or Wave6;
- Programming skills in Matlab/Python
- Knowledge of FEMAP, IMAT and Matlab
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