Published June 2025 | Version Published
Journal Article Open

Heaterless LaB₆ lollipop hollow cathode for center-mounting in Hall thrusters

  • 1. ROR icon Jet Propulsion Lab
  • 2. ROR icon California Institute of Technology
  • 3. ROR icon University of Stuttgart
  • 4. Vast, Long Beach, CA, USA

Abstract

Hollow cathodes are a critical component of Hall thrusters, providing electrons for both plasma generation and beam neutralization. A new 10-kW-class thruster, named the H10, has been developed at JPL and demonstrated >3000 s Isp and over 70 % efficiency in steady state operation at up to 15 kW. The cathode for the H10 thruster is a heaterless lanthanum hexaboride (LaB6) hollow cathode designed in a “lollipop” configuration and center-mounted in the Hall thruster. This shape features a short, compact cathode body that contains the LaB6 thermionic insert, graphite keeper and alumina insulators. The cathode assembly then necks down to a small diameter gas feed tube that acts as the cathode electrical conductor, and a separately insulated keeper lead. This geometry is ideally suited for magnetically shielded Hall thrusters because it minimizes the amount of magnetic material that must be removed from the inner magnetic core to fit in the centrally-mounted cathode, thus enabling higher magnetic fields by reducing saturation of the inner core. The heaterless cathode starts in only 3 min using less than 100 W of keeper discharge power, and has demonstrated operation in the thruster at discharge currents of 2–50 A. The design, performance and life of the cathode and heater are described.

Copyright and License

© 2025 The Authors. Published by Elsevier Ltd on behalf of IAA. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

Acknowledgement

The research described in this paper was carried out by the Jet Propulsion LaboratoryCalifornia Institute of Technology, under a contract with the National Aeronautics and Space Administration (80NM0018D0004), and was funded through the internal JPL Research and Technology Development program. © 2024. California Institute of Technology.

Conflict of Interest

All authors have no financial and personal relationships with other people or organizations that could inappropriately influence or bias this work.

Additional Information

No generative AI or AI assisted technologies were used in any way in the preparation of the manuscript.

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Additional details

Funding

Jet Propulsion Laboratory
National Aeronautics and Space Administration
80NM0018D0004

Dates

Submitted
2025-01-22
Accepted
2025-02-26
Available
2025-02-28
Available online
Available
2025-03-04
Version of record

Caltech Custom Metadata

Caltech groups
Division of Engineering and Applied Science (EAS)
Publication Status
Published