Bachelor’s degree in mechanical, aerospace, or other relevant engineering discipline
8+ years of hands-on laboratory or work experience in optomechanics, electromechanical mechanisms, or electrical/mechanical design and testing
Deep experience with CAD and FEA software packages (examples/ NX, Simcenter, FEMAP, and/or Hypermesh)
Minimum 3+ years of experience working with one or more computer programing languages (examples: Python, Rust, C++, and/or MATLAB)
Experience with precision optical mechanisms — specifying requirements, trading gimbal / head-mirror / nested coarse-fine architectures, quantifying mechanism error, and validating pointing performance at the system level
Deep knowledge of 2-axis gimbal design for space applications, including bearing selection and preload, structural design, drive mechanisms, angular runout, and long-life operation in vacuum
Experience closing line-of-sight performance budgets through analysis, controls integration, and test — including structural dynamics, tolerance stack-up, jitter analysis, pointing calibration, and environmental qualification
Familiarity with precision actuation, sensing, and control technologies for space mechanisms, including encoders, resolvers, gyros / IMUs, and feedforward / closed-loop control approaches
Experience designing harness routing, cable wraps, slip rings, and other cable-management approaches for continuously or widely rotating mechanisms, including routing optical fibers through moving axes while managing bend radius, strain relief, and pointing disturbance
Experience leading mechanism hardware through the full product life cycle: requirements generation, architecture trades, detailed design, prototype builds, assembly / integration / test, productionizing, and flight validation
Experience contributing to spacecraft-level alignment and calibration planning for optical pointing mechanisms, including coordination with optical, GNC, and systems teams to relate mechanism reference frames to payload, spacecraft, and star-tracker coordinate systems
Experience with NASA-STD-5017, SMC-S-016, and GSFC-STD-7000 for the design and qualification of in-space Moving Mechanism Assemblies