Lead, Systems Engineering Space Vehicle Bus Integration & Test

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:

• Bachelors 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