Side feeding mechanism for micro cathode arc thruster

The primary focus of this work is to characterize a micro-cathode arc thruster with a propellant feeding mechanism to extend its lifetime. To that end, we have proposed a side-feeding micro-cathode arc thruster. The thruster’s in-built feeding mechanism allows the cathode to be consumed during operation, providing a continuous supply of propellant. The ion-to-arc current fraction of about 0.025 was detected, and an initial pulse count of 1.34 M was achieved, demonstrating the effectiveness of the feeding mechanism. An average erosion rate of 4 µg/C was measured, and a total change in cathode length of 10 mm indicates the successful implementation of the spring-loaded side feeding mechanism.

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Publication Details

Journal
Journal of Electric Propulsion
Published
2025-03-11
DOI
https://doi.org/10.1007/s44205-025-00116-2
Primary Topic
Vacuum and Plasma Arcs
Type
article
Field-Weighted Citation Impact
0.00

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article

Side feeding mechanism for micro cathode arc thruster

Anmol Taploo, Guru Sankar Duppada, Michael Keidar, Vikas Soni et al.
2 links
Journal of Electric Propulsion
Vacuum and Plasma Arcs
article

Side feeding mechanism for micro cathode arc thruster

Anmol Taploo, Guru Sankar Duppada, Michael Keidar, Vikas Soni, Jake Spinelli, Adam Karp
article en

Abstract

The primary focus of this work is to characterize a micro-cathode arc thruster with a propellant feeding mechanism to extend its lifetime. To that end, we have proposed a side-feeding micro-cathode arc thruster. The thruster’s in-built feeding mechanism allows the cathode to be consumed during operation, providing a continuous supply of propellant. The ion-to-arc current fraction of about 0.025 was detected, and an initial pulse count of 1.34 M was achieved, demonstrating the effectiveness of the feeding mechanism. An average erosion rate of 4 µg/C was measured, and a total change in cathode length of 10 mm indicates the successful implementation of the spring-loaded side feeding mechanism.

Journal of Electric PropulsionVol. 4(1)
George Washington University (US)
Air Force Office of Scientific Research
Openalex Percentile: Top 97%
Vacuum and Plasma Arcs
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Side feeding mechanism for micro cathode arc thruster — Anmol Taploo, Guru Sankar Duppada, et al. · Journal of Electric Propulsion (2025) | TGRS Research Map | TGRS