Enhancing Confinement and Acceleration of Cathodic Plasma Plume by Using Electro-magnetic Nozzle
ORAL
Abstract
The EMN is demonstrated with a gridded hollow cathode and with argon as working gas. [5] The measurement of near-field plasma is performed with a Langmuir probe and Faraday probe. The formation of virtual cathode on the axis of the plume is observed when the B field at the throat is larger than 50 G, which indicates effective electron confinement. Ion flux density is greatly enhanced when the positive bias is applied on ring-electrode. The results prove the concept of EMN on plasma confinement and acceleration for propulsive applications.
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Publication: [1] Takahashi, K. "Helicon-type radiofrequency plasma thrusters and magnetic plasma nozzles," Rev. Mod. Plasma Phys. 3, 3 <br> (2019). https://doi.org/10.1007/s41614-019-0024-2<br>[2] Takahashi, K., Sugawara, T. & Ando, A. "Spatially- and vector-resolved momentum flux lost to a wall in a magnetic nozzle rf <br> plasma thruster". Sci Rep 10, 1061 (2020).<br>[3] Takahashi, K., Charles, C., Boswell, R. W., and Ando, A., "Thermodynamic Analogy for Electrons Interacting with a Magnetic <br> Nozzle," Phys. Rev. Lett. 125, 165001 (2020) https://doi.org/10.1103/PhysRevLett.125.165001 <br>[4] Correyero, S., Jarrige, J., Packan, D., and Ahedo, E., "Plasma beam characterization along the magnetic nozzle of an ECR <br> thruster," Plasma Sources Sci. Technol. 28 095004 (2019), https://doi.org/10.1088/1361-6595/ab38e1<br>[5] Chan, Y.A., Edamoto, M., Romano, F., Herdrich, G., Yamamoto, N. "Electro-magnetic Nozzle for Plasma Acceleration of an <br> Inertial Electrostatic Confinement Cathode: Development and Characterization," 7th Space Propulsion Conference, <br> SP2020_00308, virtual, March 17 – 19, 2021
Presenters
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Yung-An C Chan
Institute of Space Systems, University of Stuttgart
Authors
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Yung-An C Chan
Institute of Space Systems, University of Stuttgart
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Georg Herdrich
Institute of Space Systems, University of Stuttgart