Lead, Systems Engineering - Space Vehicle Bus Integration & Test

L3

Harris 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. L3

Harris 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.

L3

Harris 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 Code: 42141

Job Location:

Palm Bay, Florida

Job Schedule:

9/80 Regular

This technical-lead role provides Space Vehicle bus integration and test leadership for Moog buses. The lead is the primary technical coordinator for bus and TT&C suppliers, directs Bus environmental verification test readiness and execution, and integrates bus-level requirements, interfaces, verification, and anomaly resolution across the development, integration, and production lifecycle.

• Lead SV-bus I&T planning and execution across electrical power, attitude control, TT&C, C&DH, and other bus-to-payload/system interfaces.
• Serve as the technical point of contact for bus and TT&C suppliers; establish technical baselines, flow down requirements, resolve interface issues, and contribute to supplier and program technical reviews.
• Coordinate Bus environmental verification test readiness, integration, test procedures, readiness reviews, test-data disposition, and closure of verification evidence.
• Maintain requirements, interface, and verification traceability; assess impacts of changes across bus, payload, ground, and mission interfaces.
• Lead investigation and resolution of anomalies, nonconformances, and technical risks, including root-cause/corrective-action closure and lessons learned.
• Partner with systems engineering, hardware, software, quality, manufacturing, and operations teams to transition bus capabilities through first-unit build, development test, integration, and production.
• Communicate technical status, decisions, risks, and recovery plans to program leadership and customers; mentor engineers in disciplined I&T execution.

• Bachelor's Degree and a minimum of 9 years of prior relevant experience;
  Graduate Degree and a minimum of 7 years of prior related experience; or, in lieu of a degree, a minimum of 13 years of prior related experience.
• Demonstrated experience in space-vehicle bus systems engineering, integration, and test, including technical ownership of subsystem and system interfaces.
• Working knowledge of SV bus subsystems such as electrical power, attitude control, TT&C, C&DH, structures, thermal, and avionics, with the ability to resolve cross-domain interface issues.
• Experience with requirements development and flowdown, interface management, verification planning and execution, test readiness, and test-data review in a hardware development program.
• Experience leading or coordinating suppliers and multidisciplinary engineering teams through technical decisions, anomaly resolution, and corrective actions.
• Active Top Secret/Sensitive Compartmented Information (TS/SCI) security clearance.
• Ability to obtain and maintain Special Access Program (SAP) access, as required.

• Experience with DOORS, RVTM, or comparable requirements and verification-traceability tools.
• Experience with model-based systems engineering, SysML, or architecture models used to…