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Provide Satellite and Payloads Architecture for Electrical Power design and EMC, including bus power sizing, definition, performance analysis, implementation, and validation in support of the Satellite System Engineering Team. Tasks include complete electrical, EMC, and harness design, verification and validation of electrical and power architecture, satellite bus power sizing suitable to particular missions, and definition of power systems from solar arrays to battery. You will support mission analysis & requirements, define, analyze, and write requirements definition, SOC, verification and validation matrix, design description, systems budgets, equipment specifications, and test requirements for the power sub-systems based on mission requirements. Additionally, you will provide inputs and support to all program reviews (EQSR, SRR, PDR, CDR), attend test reviews (TRR, TRB, DRB, NCR's), support sub-system assembly, integration and test activities, support satellite testing (EGSE, test supervision, data analysis), support satellite tests at test facilities or supplier premises, write up the subsystem operations manual, and support In-Orbit Test (IOT).