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.
Authors
- Anmol Taploo (ORCID: https://orcid.org/0000-0003-4028-6851)
- Guru Sankar Duppada (ORCID: https://orcid.org/0000-0003-1432-8755)
- Michael Keidar (ORCID: https://orcid.org/0000-0003-0869-4310)
- Vikas Soni (ORCID: https://orcid.org/0000-0002-0729-4641)
- Jake Spinelli
- Adam Karp
Institutions
- George Washington University (US)
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
Funders
- Air Force Office of Scientific Research