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Job Title: Lead, Systems Engineering - Space Vehicle Bus Integration & Test
Job Code: 42141
Job Location: Palm Bay, Florida
Job Schedule: 9/80 Regular
Job Description:
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.
Essential Functions:
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.
Qualifications:
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
Preferred Additional Skills:
Experience with DOORS, RVTM, or comparable requirements and verification-traceability tools.
Experience with model-based systems engineering, SysML, or architecture models used to manage SV interfaces.
Experience coordinating environmental, development, qualification, acceptance, or production test for space-vehicle hardware.
Experience preparing for and conducting system, supplier, test-readiness, and flight-readiness reviews.
Experience with supplier technical management, failure review, root-cause/corrective-action methods, and risk-recovery planning.
LI-LS4
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Please be aware many of our positions require the ability to obtain a security clearance. Security clearances may only be granted to U.S. citizens. In addition, applicants who accept a conditional offer of employment may be subject to government security investigation(s) and must meet eligibility requirements for access to classified information.
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