Job Description:
What you'll do:
- Actuated System Layouts: Develop and mature system layouts and installation concepts for actuators, mechanisms, linkages, brackets, mounting provisions, and associated hardware within vehicle packaging constraints.
- Mechanical Design Ownership: Own detailed CAD design of actuated systems hardware from concept through drawing release, including load paths, materials, interfaces, GD&T, and tolerance stack-ups.
- Actuator and Mechanism Integration: Perform actuator sizing, kinematic layout, and installation analysis for flight control surfaces, bay doors, and other airframe mechanisms.
- Installation Analysis: Perform hand calculations and basic FEA to substantiate brackets, mounts, linkages, and mechanical installation hardware.
- Vehicle Interfaces: Define and resolve installation interfaces with structures, EWIS, EPS, thermal management, and adjacent systems, including routing, clearances, and maintainability provisions.
- Design Documentation: Develop and maintain CAD models, drawings, interface definitions, and design data packages to program standards for SRR, PDR, and CDR.
- Hardware and Supplier Execution: Support component selection, technical specifications, supplier technical execution, prototype assembly, and mechanical test-fixture development.
- Qualification and Hardware Delivery: Define and execute qualification test plans per MIL-STD-810, using results to mature the design into production-ready hardware and support MIL-HDBK-516 Airworthiness Certification.
Required qualifications:
- Experience: 5 to 12 years of mechanical systems design experience in aerospace or a comparable regulated industry, with hands-on experience designing actuated mechanisms or aircraft installations.
- Education: B.S. or M.S. in Mechanical Engineering, Aerospace Engineering, or a related technical discipline.
- Core Fundamentals: Deep mastery of mechanical design, kinematics, load paths, materials selection, GD&T, and tolerance stack-up methodologies.
- Analysis and Modeling: Demonstrated capability performing closed-form hand calculations and basic FEA for mechanisms, brackets, mounts, and structural installation components.
- CAD and PLM: Extensive experience in 3D CAD modeling, mechanical layouts, and drawing release, with Siemens NX, CATIA, Creo, or equivalent PLM workflows.
- Actuated Systems Integration: Demonstrated ability to develop actuator and mechanism installations that satisfy packaging, load, clearance, maintainability, and vehicle-interface requirements.
- Hardware and Supplier Execution: Proven track record sourcing COTS/custom aerospace components, driving suppliers to schedule, and assembling benchtop or vehicle-level test setups.
- Autonomy: Demonstrated ability to self-direct, prioritize technical tasks without oversight, and deliver functional hardware under tight timelines.
- Clearance eligible
Preferred qualifications:
- Aircraft flight control actuation, weapons bay door, landing gear, or other deployable-mechanism design experience.
- Experience with electro-mechanical or electro-hydrostatic actuation systems.
- Familiarity with MIL-HDBK-516, MIL-STD-810, and airworthiness verification planning for mechanical systems.
- Hands-on machine shop, fabrication, mechanical assembly, or prototype-build experience in a rapid R&D environment.
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