Operation of a plasma thruster featuring a 1.1 T high temperature superconducting magnet

Abstract Increasingly ambitious space missions rely upon the advancement of propulsion systems, and innovations in electric propulsion represent a vital step toward potential solutions. Electric propulsion research has indicated improved thruster performance at higher magnetic fields, but real-world implementations have been encumbered by available magnet technology. In this study, a new class of superconducting magnet designed for such space applications is demonstrated. A central cathode electrostatic thruster was paired with a conduction cooled high temperature superconducting magnet operated in non-pulsed mode. Using Xe propellant, thrust of 38–73 mN was measured at a central bore magnetic field of 1.13 T and on-anode field of 1.28 T, and the thruster’s specific impulse was throttled between 1050s and 1450s. The peak thruster efficiency was 18.7%, inclusive of the power consumption of the magnet subsystems. This was performed without the onset of plasma instabilities, and is the first case in the literature of a high temperature superconducting plasma thruster operating at >1 T.

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Publication Details

Journal
Journal of Electric Propulsion
Published
2024-09-13
DOI
https://doi.org/10.1007/s44205-024-00080-3
Citations
10
Primary Topic
Plasma Diagnostics and Applications
Type
article
Field-Weighted Citation Impact
2.09

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article

Operation of a plasma thruster featuring a 1.1 T high temperature superconducting magnet

Daisuke Ichihara, Nicholas J. Long, Kiyoshi Kinefuchi, Cameron Shellard et al.
10 citations
Journal of Electric Propulsion
Plasma Diagnostics and Applications
2.09
article

Operation of a plasma thruster featuring a 1.1 T high temperature superconducting magnet

Daisuke Ichihara, Nicholas J. Long, Kiyoshi Kinefuchi, Cameron Shellard, Stuart C. Wimbush, Nick Strickland, Jamal R. Olatunji, Betina Pavri, Max Goddard-Winchester, Jakub Głowacki, Chris R. Acheson, Ryota Nakano, Konstantinos Bouloukakis, Randy Pollock, Daiki Maeshima, Ryoyu Mori, Ryohei Takagi
article en
10 citations

Abstract

Abstract Increasingly ambitious space missions rely upon the advancement of propulsion systems, and innovations in electric propulsion represent a vital step toward potential solutions. Electric propulsion research has indicated improved thruster performance at higher magnetic fields, but real-world implementations have been encumbered by available magnet technology. In this study, a new class of superconducting magnet designed for such space applications is demonstrated. A central cathode electrostatic thruster was paired with a conduction cooled high temperature superconducting magnet operated in non-pulsed mode. Using Xe propellant, thrust of 38–73 mN was measured at a central bore magnetic field of 1.13 T and on-anode field of 1.28 T, and the thruster’s specific impulse was throttled between 1050s and 1450s. The peak thruster efficiency was 18.7%, inclusive of the power consumption of the magnet subsystems. This was performed without the onset of plasma instabilities, and is the first case in the literature of a high temperature superconducting plasma thruster operating at >1 T.

Journal of Electric PropulsionVol. 3(1)
Victoria University of Wellington (NZ), Nagoya University (JP)
Ministry of Business, Innovation and Employment, Japan Society for the Promotion of Science
Openalex Percentile: Top 12%
Plasma Diagnostics and Applications
2.09
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