Specialist, Mechanical Engineer - Structural Analyst (Space Systems) (ROCHESTER)

L3Harris is dedicated to recruiting and developing high-performing talent who are passionate about what they do. Our employees are unified in a shared dedication to our customers’ mission and quest for professional growth. L3Harris provides an inclusive, engaging environment designed to empower employees and promote work-life success. Fundamental to our culture is an unwavering focus on values, dedication to our communities, and commitment to excellence in everything we do.

L3Harris is the Trusted Disruptor in defense tech. With customers’ mission-critical needs always in mind, our employees deliver end-to-end technology solutions connecting the space, air, land, sea and cyber domains in the interest of national security. Job Title: Specialist, Mechanical Engineer – Structural Analyst (Space Systems) Job Code: 37545 Job Location: Rochester, NY or Wilmington, MA Job Schedule: 9/80 (Every other Friday off) Relocation: Relocation assistance is available to qualified applicants

Job Description: The L3Harris space superiority and imaging mechanical engineering department is seeking a structural analyst to join our team and support programs that we have recently won. The department specializes in space-based, small and large aperture visible and IR telescopes with integrated electromechanical devices used for motion and focus control.

In this role you will perform structural analysis of complex space systems including optomechanical assemblies, precision structures, mechanisms, and electronic packaging. This position requires independent execution of sophisticated analyses, technical leadership, and collaboration across multidisciplinary teams to ensure structural integrity and system performance from concept through flight.

Essential Responsibilities Interpret system specifications to develop achievable analysis plans Develop finite element models of complex space structures, including composites, metallics, and glass Perform comprehensive analyses for structural responses to ground, test, launch, and on-orbit environments, including: Structural strength and stability, Modal characteristics and dynamic response, Vibroacoustic environments, Thermoelastic response, Optomechanical performance, Fatigue/fracture assessments. Validate analysis approaches through correlation with test data and hand calculations Work independently with minimal oversight Prepare technical reports, analysis documentation, and presentations for internal reviews and customer deliverables Support design reviews, trade studies, and design optimization efforts Interface directly with design engineers, systems engineering, and test organizations Contribute throughout the development cycle: requirements definition, concept trades, preliminary/final design, component selection, and integration/test support Support manufacturing operations and provide technical guidance Participate in risk identification and mitigation activities Selected candidate will need to be able to obtain a U.S. security clearance

Qualifications: Bachelor’s Degree in Mechanical Engineering or other related engineering or science degree and minimum 4 years of prior relevant experience. Graduate Degree and a minimum of 2 years of prior related experience. In lieu of a degree, minimum of 8 years of prior related experience. 2+ years experience with FEA codes (Nastran preferred; Ansys or Abaqus also considered) and pre/post processors (Femap or Patran preferred) Professional experience with structural analysis methods (FEA and hand-calculations) Professional experience with structural analysis of aerospace systems

Preferred

Additional Skills: Active TS/SCI Clearance is preferred Experience in the structural analysis of space structures Optomechanical systems and precision structures Composite structure design and analysis Dynamic analysis and test (modal, sine, random, acoustic, shock) Launch loads derivation and analysis Fracture and damage tolerance analysis Jitter/vibration analysis On-orbit Structural-Thermal-Optical-Performance (STOP) analysis Familiarity with NASA or DoD structural design standards and requirements Programming/scripting experience (MATLAB, Pyth