Description
The Electrical Propulsion Engineer will translate mission-level delta-v, thrust, lifetime, and reliability goals into electrical propulsion system requirements and detailed design documents. The role covers power, thermal, mass, and contamination budgets; thruster, PPU, propellant-handling, and control-system design; modeling and simulation; FDIR and telemetry interfaces; integration and verification testing; launch, on-orbit, and operations support; and technical leadership. It requires a B.Sc. in Electrical Engineering, Aerospace, or Physics and at least 8 years of electrical propulsion engineering experience on LEO/MEO platforms.
