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Lead, Mechanisms Mechanical Engineer; Space Systems

Job in Wilmington, Middlesex County, Massachusetts, 01887, USA
Listing for: L3Harris Technologies
Full Time position
Listed on 2025-12-24
Job specializations:
  • Engineering
    Mechanical Engineer, Systems Engineer
Salary/Wage Range or Industry Benchmark: 150000 - 200000 USD Yearly USD 150000.00 200000.00 YEAR
Job Description & How to Apply Below
Position: Lead, Mechanisms Mechanical Engineer (Space Systems)

Lead, Mechanisms Mechanical Engineer (Space Systems)

Join to apply for the Lead, Mechanisms Mechanical Engineer (Space Systems) role at L3

Harris Technologies

Job Location

Wilmington, MA

Job Schedule

9/80 (Every other Friday off!)

Relocation Assistance

Relocation assistance is available to qualified applicants.

Job Description

L3

Harris is seeking a highly skilled and dynamic senior Mechanical Engineer to support customer-funded programs and internal research efforts within our Space, Superiority and Imaging Division. Our Intelligence, Surveillance, and Reconnaissance solutions serve a broad array of government, civil, and commercial customers by enhancing information superiority, contributing to our national security and providing actionable data for the protection of property and human life.

We specialize in high-reliability airborne and space-based remote sensing payloads that offer active and motion imaging and data processing, exploitation and dissemination. We also provide solutions that map and monitor the earth for a variety of commercial and governmental users. Mechanical Engineer to perform design, development, analysis, and manufacturing tasks on complex mechanical hardware including precision space structures and mechanisms in a program team environment.

Program support and technical leadership over requirements definition, concept generation, material and finish selection, trade studies, design sensitivity/optimization studies, preliminary and detailed design, design sensitivity and tolerance analysis, design documentation, Bill of Materials (BOM) management, and assembly/integration and testing. Candidate must have strong proficiency in 3D modeling, design for manufacturing, and ability to work independently or within a multi-disciplined team environment.

Responsibilities
  • Design high-precision and complex space opto-mechanical telescopes hardware as part of an Integrated Product Team (IPT). Hardware variety spans machined components, composite structures, deployable mechanisms, opto-mechanical support structure, and thermal blankets
  • Leverage high reliability, flight-proven, heritage design concepts in order to produce high quality designs within an aggressive timeline
  • Interface with outside suppliers/customers and other engineering disciplines to drive designs to closure (Structural, Thermal, Electrical, Manufacturing, Integration and Testing, Quality, Configuration Management).
  • Present design details at program reviews to customers and independent reviewers.
  • Develop and perform testing to show proof-of-concept and/or qualification of new designs.
  • Support production operations with design of tooling, test equipment, and shop aids.
  • Provide regular status updates to Program Management and Project Engineers on cost and schedule performance.
  • Responsible for establishing key performance error budgets
  • Identify and select mechanism components like ball bearings, motors (servo, stepper, limited-angle torque, solenoids, and voice coils), position sensors (encoders, resolvers, LVDTs, Hall effect), and springs
  • Calculates torque margin per AIAA S-114A-2020 and/or NASA-STD-5017
  • Design launch lock solutions for mechanisms, particularly for low shock and FOD containment
  • Selecting lubricants for spaceflight applications near sensitive optics
  • Work on designs for vacuum environments over broad temperature ranges while maintaining cleanroom cleanliness
  • Defines and establishes the technical approach to meet assigned objective.
  • Prepares reports, formal documentation and presentation materials summarizing analysis results and present results to both external and internal groups, including leadership and customers including Preliminary Design reviews (PDR), Critical Design Reviews (CDR) and Technical Interchange Meetings (TIM)
Qualifications
  • Bachelor’s Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience.
  • 6+ years in CAD modeling and design tools
  • Prior or current experience with spaceflight mechanism applications, especially related to optical systems
  • 5+ years of professional experience…
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