Bachelor’s degree in mechanical, aerospace, or other relevant engineering discipline
5+ years of hands-on laboratory or work experience in optics, laser technology, controller development, electromechanical mechanisms, or electrical/mechanical design or testing
Deep Experience with CAD and FEA software packages (examples/ NX, Simcenter, FEMAP, and/or Hypermesh)
Minimum 2 years of experience with working with computer programing language (examples/ Python, Rust, C++, and/or MATLAB)
Experience designing and manufacturing flexure-guided mechanisms that provide deterministic constraint, low-friction motion, high repeatability, and controlled stiffness across translational and rotational degrees of freedom
Experience designing voice-coil or piezo driven mechanisms and methods for elegantly integrating positional feedback
Experience with electronic enclosure packaging of printed circuit boards for space applications
Direct experience developing fine-pointing and line-of-sight stabilization solutions for payloads such as optical communication, EO/IR sensors, antennas, or telescopes
Perform detailed mechanical analysis (FEA, tolerance stack-up, kinematic modeling, vibration/shock analysis) to ensure performance under extreme environments (thermal vacuum, high-g during launch, vibration and jitter)
Experience collaborating with electrical, controls, and optical engineers to close multi-disciplinary performance loops (pointing accuracy, jitter, settling time, bandwidth)
Create and maintain detailed CAD models, drawings, and BOMS (NX preferred)
Experience leading prototyping, assembly, integration and test activities, including environmental qualification testing
Detailed knowledge and experience implementing control loops for mechanism angle utilizing both feed forward and closed loop sensors (PID, adaptive, model predictive MPC)
Deep knowledge of high-resolution encoders, resolvers, gyros/IMUS/SIRU for space applications
Experience with NASA-STD-5017, SMC-S-016, and GSFC-STD-7000 for the design and qualification of in-space Moving Mechanism Assemblies