Assess structural elements of satellite systems for static and dynamic responses
Iterate through design options, both in simulation and test, to rapidly enhance confidence in hardware
Identify requirement verification methods and establish plans to mitigate technical risks through combinations of Calculation, FEA, Test, etc.
Identify, recommend, and implement design changes in CAD to ensure system survivability and performance
Support hands-on work building and testing hardware at both prototype and flight levels
Generate documentation required to substantiate designed solutions and adequately communicate them to stakeholders
Act as peer or lead reviewer providing technical oversite or subject matter expertise on other active designs
Requirements
5+ years of relevant mechanical design experience
Bachelor's degree in mechanical engineering, mechatronics engineering, or equivalent
Understanding of design principles for heat transfer, temperature control, statics, and dynamics
Experience in verifying designs through Finite Element Analysis and testing
Experience with one or more CAD tools (Onshape, Creo, Solidworks, etc.)
Understanding of design for manufacturing and assembly practices
Strong communication and documentation skills working in a multidisciplinary team
Comfortable in an R&D lab environment
Comfortable using basic hand and power tools
Bonus: Knowledge and/or experience in design for space applications, specifically vibration simulation and testing for satellite and unit development and qualification
Bonus: In-depth experience using Simcenter (NX) NASTRAN and Response Dynamics module
Bonus: Familiarity with ESA ECSS or NASA structural design and testing standards