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Blue Origin

Aerospace Systems Engineer III (Structures & Mechanisms)

1w

Blue Origin

Cape Canaveral, US · Full-time · $121,023 – $169,432

About this role

At Blue Origin we develop reusable space vehicles within a culture of safety and collaboration. This role is part of the Lunar Permanence business unit building sustainable infrastructure for crew and cargo transport to the lunar surface. The Aerospace Systems Engineer III owns requirements and verification for structural and mechanical elements of lunar flight hardware.

Daily work includes developing and allocating subsystem requirements while maintaining traceability to mission objectives. You define interfaces across mechanical electrical and software boundaries and execute integration across design analysis manufacturing and test teams. Verification strategies are planned with the verification team using test analysis inspection or similarity methods.

You partner with Structures Mechanisms Avionics Thermal GN&C Propulsion Manufacturing and Test teams to deliver flight-ready hardware. The position addresses lunar environments including thermal extremes dust vacuum launch loads and landing shock. Technical reviews such as SRR PDR CDR TRR and FRR are supported with status on requirements verification and risks.

Root cause analysis is performed on anomalies through FRACAS activities with corrective actions implemented to prevent recurrence. Systems engineering processes are improved in areas of requirements quality configuration control and interface management. This work directly advances Blue Origin's mission of enabling millions of people to live and work in space.

Requirements

  • B.S. in Aerospace Engineering Mechanical Engineering or related field.
  • 7+ years of aerospace systems engineering experience in requirements integration and verification.

Responsibilities

  • Develop decompose allocate and manage requirements for structural and mechanical subsystems with end-to-end traceability to lunar mission objectives.
  • Define and control interfaces across mechanical electrical software and ops boundaries including vehicle-to-payload and vehicle-to-ground equipment.
  • Plan and execute subsystem integration for structures and mechanisms coordinating across design analysis manufacturing assembly and test.
  • Define verification strategies and methods then author and approve verification plans to drive closure with objective evidence.
  • Ensure design and verification approaches address lunar environments including thermal extremes dust vacuum launch loads and landing shock.
  • Lead anomaly investigations and FRACAS activities performing root cause analysis and implementing corrective actions.
  • Support technical reviews and readiness milestones presenting requirements status verification status risks and interface readiness.