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L3Harris Chief Mechanical Engineer – Space Vehicle Mechanical in Palm Bay, Florida

Description:

Job Title: Chief Mechanical Engineer – Space Vehicle Mechanical

Job Code: SAS20201412-54199

Job Location: Palm Bay, FL

Job Description:

This position will be responsible for providing Mechanical Systems Engineering support for space vehicles and associated subsystems across multiple responsive space programs in the Space and Airborne Systems Segment of L3Harris Technologies.

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.

Learn more about the small satellite solutions we provide for government and commercial organizations here: https://www.l3harris.com/capabilities/space

Mechanical Systems Engineer to oversee and lead the mechanical system requirements, design, development and analysis tasks for complex novel spacecraft design hardware including space structures, space antenna systems, launch vehicle interfaces, payload to bus interfaces, and complex electronic packaging in a program team environment. Program support and technical leadership over requirements definition, concept generation, material selection, trade studies, design sensitivity/optimization studies, preliminary and final design, design documentation, and assembly/integration and testing. Candidate must have strong proficiency in requirements definition and control, spacecraft bus system experience, launch vehicle interface experience, design for manufacturing, and ability to work independently in or leading in a multi-disciplined team environment.

  • Coordinate with System Integration and Test engineer responsible for the assembly, integration, and testing of payload & space vehicle software and mechanical aspects such as subsystems including power, attitude control, T&C (Telemetry & Command), C&DH (Command & Data Handling), and inter-subsystem interfaces to ensure all mechanical engineering requirements are met

  • Work with and ensure collaboration between a variety of Subject Matter Experts (SMEs) in various space vehicle subsystems and environments (thermal, EMI/EMC/ESD, dynamics etc.)

  • Perform hardware/software requirements definition, decomposition, allocation, management, verification, and validation

  • Work with SMEs to define and ensure mechanical interface requirements are properly flowed down to each subsystem and coordinated between subsystems including key suppliers such as for bus components or subsystems

  • Define and establish spacecraft technical baseline to meet program customer requirements.

  • Work with SMEs to ensure subsystem verification testing and analysis is performed with appropriate modeling of inter-subsystem interfaces

  • Participate and present information for internal and external technical reviews including peer reviews, requirements reviews, design reviews, qualification reviews and customer System Requirements Review (SRR), Preliminary Design reviews (PDR), Critical Design Reviews (CDR) and Technical Interchange Meetings (TIM)

  • Support subsystem and system level mechanical testing including data reviews, anomaly investigations and RCCA (Root Cause Corrective Action) closure

  • Contribute to the development of detailed work instructions, processes and procedures directing the assembly and test of launch space vehicle (SV) systems, ensuring consistent application of assembly processes and philosophies across all products

  • Support program technical and management leadership, as required

  • Support and lead technical discussions with customers, as required

Qualifications:

  • Bachelor’s Degree and a minimum of 12 years of prior relevant experience. Graduate Degree and a minimum of 10 years of prior related experience.

  • 10 + years experience in a mechanical engineering or systems engineering role in one or more space vehicle subsystems

  • 10 + years experience in spacecraft mechanical systems engineering

  • 5 + years experience leading spacecraft mechanical engineering designs

  • 5 + years experience leading multi-disciplinary mechanical engineering team through system requirements, design, analysis, test, hardware build, delivery and launch

Preferred Additional Skills:

  • Ability to perform in-depth technical work while being able to communicate effectively with multiple disciplines, program office personnel and customers

  • Organization skills to be able to lead multi-discipline teams and driving to proper technical closure while managing schedule, cost and customer expectations

  • Ability to identify any gaps in technical coverage to appropriate leadership during all phases of program execution; help fill-in any gaps, when possible

  • Detailed engineer but big thinker

  • Experience interfacing directly with customers (both prime contractors and end customers) on resolving in-depth technical issues

  • Experience executing commercial, firm-fixed price development programs for space

  • Experience with requirements derivation and tracking using DOORs (or equivalent) including requirements verification traceability matrix (RVTM).

  • Experience in design or analysis of space based mechanical structures, electronics packaging or mechanisms, along with expert level oversight of engineering drawing development

  • Proficiency in understanding of ASME Y14.5 Geometric Dimensioning and Tolerancing standards

  • Proficiency in oversight of analysis FEA tools such as Femap, NASTRAN, ANSYS, Thermal Desktop

  • Proficiency in 3D CAD modeling in Creo Parametric

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