Spacecraft represent the most pressing unmet need across the entire aerospace industry. As more launch vehicles come online and the cost to orbit decreases, more companies launching payloads to space continue to emerge. For the first time in history, this influx of payload companies combined with reduced launch costs has resulted in a massive increase in need for commercial spacecraft platforms, known as satellite buses. These buses hold the payloads of our customers and are flown on launch vehicles. Apex manufactures these satellite buses at scale using a combination of software, vertical integration, and hardware that is designed for manufacturing. Our spacecraft enable the future of society: ranging from earth observation to communications and more. Apex is seeking a Senior Electric Propulsion Engineer with deep expertise in cathodes to own the design, development, qualification, and production of cathode technology for our electric propulsion systems. Building on Apex's in-house Hall-effect thruster capability, you will drive hollow and heaterless cathode development, from emitter physics and thermal-mechanical design through cathode-thruster coupling, life characterization, and design-for-manufacturing at rate.
Responsibilities:
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- Own the end-to-end design and development of hollow and/or heaterless cathodes for Apex's electric propulsion systems, including emitter selection, keeper and orifice geometry, heater design, and thermal-mechanical packaging.
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- Develop physics-based and empirical models to predict cathode performance, discharge behavior, thermal margins, and life, and validate them against test data.
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- Define and execute cathode test and life-qualification campaigns, including ignition and conditioning, coupling voltage characterization, thermal cycling, plume/plasma diagnostics, wear testing, and long-duration life testing in vacuum facilities.
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- Drive cathode-thruster integration, optimizing cathode-to-anode coupling, mass flow split, and placement for overall EP system performance and stability.
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- Develop cathode erosion, poisoning, and degradation models and perform filtration and contamination-control analysis to demonstrate compliance with propulsion budgets for life, power, thermal, leak, and contamination.
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- Select emitter and structural materials and processes, including LaB6, BaO-impregnated tungsten, and refractory metals, and qualify them for spaceflight and scalable production.
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- Optimize cathode designs for performance, weight, cost, manufacturability, and repeatability, and develop the work instructions, process flows, and AI&T procedures required to build them at rate.
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- Partner with systems, power electronics, thermal, structures, and avionics teams to define interfaces, including cathode heater/keeper drive and PPU interaction, and verify requirements.
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- Support the build, integration, and test of flight hardware, as well as launch campaigns, on-orbit performance evaluation, and anomaly resolution.
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- Lead and contribute to failure analysis, root-cause investigations, and continuous design improvements to support future builds and scalable production.
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- Provide technical mentorship to propulsion engineers and contribute to the continued development of Apex's cathode and electric propulsion capability.
Requirements:
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- Bachelor's degree in aerospace, mechanical, electrical, plasma/propulsion engineering, applied physics, or a related field.
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- 6+ years of relevant electric propulsion experience with a Bachelor's or Master's degree, OR a Ph.D. in electric propulsion, plasma physics, applied physics, or a closely related field with 3+ years of relevant industry experience, with substantial and demonstrable focus on cathode design, development, and testing.
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- Deep, hands-on knowledge of hollow and/or heaterless cathode physics, including thermionic emission, emitter materials, plasma discharge behavior, keeper/orifice design, and cathode coupling to Hall or ion thrusters.
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- Experience planning and executing cathode or EP test campaigns in vacuum facilities, including plasma diagnostics, performance measurement, and life/wear testing.
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- Strong understanding of the failure and degradation mechanisms that drive cathode life, including emitter depletion, erosion, poisoning, and contamination, and how to design and test against them.
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- Working knowledge of spacecraft propulsion system architecture, propellant feed systems, and PPU interaction.
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- Experience owning hardware through design, development, build, and test.