Sr. Engineer, Deployment Mechanism – TeraWave Solar Array

Application close date:

Applications will be accepted on an ongoing basis until the requisition is closed.

At Blue Origin, we envision millions of people living and working in space for the benefit of Earth. We’re working to develop reusable, safe, and low-cost space vehicles and systems within a culture of safety, collaboration, and inclusion. Join our team of problem solvers as we add new chapters to the history of spaceflight!

This role is part of Advanced Concepts and Enterprise Engineering (ACE), supporting Blue Origin’s mission of millions of people living and working in space for the benefit of Earth. The team fosters innovation and drives engineering workflows of the future, shared solutions and standards, simplicity and lower costs, and manufacturable design.

As part of a hardworking team of specialists, technicians, and engineers, you will own the design, development, and qualification of the Tera Wave solar array's deployment mechanism as its Responsible Engineer, balancing tight packaging, mass, and reliability constraints. This is a deployer that unfolds the array's solar power modules on orbit, and you will be the technical authority for its architecture, analysis, and validation strategy, reporting up through the Sr.

Manager who owns top-level wing design and delivery. You will define deployment architectures, drive rapid design-build-test cycles to burn down risk, and coordinate interfaces with the solar power module, photovoltaic assembly, and harness teams to ensure the deployer integrates cleanly into the full wing. If you thrive on hands-on problem solving, taking ownership of a complex mechanism end-to-end, and want your work to directly enable humanity's future in space, this is the role for you.

Special Mentions

• Relocation provided
• Travel expected up to 25% of the time
• Interviews will include a technical assessment

Responsibilities include but are not limited to:

• Serve as Responsible Engineer for the Tera Wave solar array deployment mechanism, owning its design, analysis, and qualification
• Lead the entire design cycle for the deployer, including trade studies, conceptual and detailed design, structural analysis, development testing, and qualification
• Define deployment architecture and validation strategy, using analysis, prototyping, and environmental testing to prove performance in the space environment
• Hands-on prototyping to quickly push the design forward on fast-moving research and development cycles, including passive actuation, motors, controls, and instrumentation as the design requires
• Perform analysis for kinematic, motor/spring/gear sizing, tolerance stacks, and structural performance as the system design requires
• Lead and technically guide other engineers designing deployment mechanism sub-components and ancillary hardware (e.g., latches, hinges, dampers, hold-down and release mechanisms), ensuring their designs integrate cleanly with the overall deployer
• Own the deployer's interfaces with the solar power module (SPM), photovoltaic assembly (PVA), and harness subsystems; coordinate with subsystem owners to resolve interface conflicts
• Drive DFM/DFA and producibility to reduce cost and meet schedule as the deployer matures toward production rate
• Generate component drawings, assembly drawings, and interface control documents with application of GD&T per ASME Y14.5
• Perform flight hardware testing: TVAC, modal, vibration, and functional deployment testing
• Own the deployer-level risk register and DFMEA; drive rapid issue resolution during integration, test, and qualification anomalies
• Collaborate in a scrappy, cross-disciplinary R&D environment, working with structural, thermal, electrical, and manufacturing disciplines to deliver a fully integrated mechanism
• Coach, mentor, and technically assist junior engineers working on the deployment mechanism

Minimum Qualifications

• Bachelor of Science degree in Mechanical Engineering, Aerospace Engineering, or a related engineering discipline; 8+ years of experience
• Recent experience designing and building mechanical hardware (passive or active mechanisms preferred)
• Hands-on prototyping and testing experience
• Strong mechanical design, integration, and mechanism analysis skills using 3D modeling (Creo preferred) and simulation tools
• Experience with GD&T per ASME Y14.5 and performing tolerance stackup analysis
• Knowledge of manufacturing, assembly, integration, and verification/qualification testing
• Familiarity with space environments, verification standards, and vacuum environments
• Desire and drive to learn new skills and technical tools as the program develops
• Must be a U.S. citizen or national, U.S. permanent resident (current Green Card holder), or lawfully admitted into the U.S. as a refugee or granted asylum.

Preferred Qualifications

• Experience with solar arrays or other large-format deployable spacecraft structures
• Experience with large-scale deployable and/or complex moving mechanisms from concept through qualification
• Experience with composites
• Deep knowledge of…