Required Experience: • Typically requires a Bachelors, Masters or PhD in engineering or a related technical field as well as eleven or more years of progressively complex engineering experience. May substitute equivalent experience in lieu of education. • Spacecraft, aerospace, defense, or other high-reliability electrical hardware development. • Electrical power system architecture, design, analysis, integration, and test, including power generation, energy storage, power distribution, power conditioning, protection, and monitoring. • Spacecraft electrical interconnect design, including harnesses, cable assemblies, connectors, grounding, bonding, shielding, and interface control. • Development and execution of electrical integration and test activities for flight hardware, engineering development units, qualification units, or equivalent high-reliability systems. • Experience leading technical teams and coordinating multidisciplinary engineering activities through design, manufacturing, integration, verification, and test. • Experience with requirements definition, verification planning, technical reviews, configuration management, and engineering documentation. • Experience troubleshooting complex electrical hardware and resolving anomalies through structured failure analysis and root-cause investigation. • Experience with electrical safety, electrostatic discharge (ESD) controls, contamination control, and handling practices for high-reliability or flight hardware. • Must be customer focused and able to work on a self-initiated basis or in a team environment and able to work extended hours and travel as required. • Active DoD Secret Clearance is required. Desired Qualifications • Experience developing spacecraft electrical power systems, including solar arrays, batteries, power distribution, converters, load switches, and battery management systems. • Experience with spacecraft interfaces and harnesses, including SpaceWire, MIL-STD-1553, CAN, Ethernet, serial interfaces, discrete I/O, connectors, shielding, grounding, bonding, fabrication, and testing. • Experience supporting environmental, qualification, and acceptance testing, including thermal vacuum, vibration, shock, EMC, and radiation testing. • Familiarity with NASA, DoD, or commercial space standards; space-qualified components; derating; reliability; and parts, materials, and process controls. • Experience with electrical design, modeling, simulation, and test tools, including Altium, AutoCAD Electrical, MATLAB/Simulink, PSpice, LTspice, LabVIEW, and Python. • Experience with power-system analysis, automated test equipment, data acquisition, hardware-in-the-loop testing, and electrical test equipment. • Experience supporting technical reviews, including SRR, PDR, CDR, TRR, qualification, and acceptance reviews. • Familiarity with configuration, requirements, and product lifecycle management tools. • Demonstrated technical leadership, project coordination, customer communication, and ability to resolve complex engineering problems.