Fundamental difference between the two Hall thruster variants

By E. Choueiri. 2001

150 citations recorded by the source corpus.

Subfields: Electrical and Electronic Engineering

View Paper: https://www.semanticscholar.org/paper/d49177d61e7b85f1547f015da1ac3e3917e84f2d

How researchers see this paper

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In Electrical and Electronic Engineering

1. S. Mazouffre
2. R. Hofer

Citations in the corpus

• Electric propulsion for satellites and spacecraft: established technologies and novel approaches (2016, background): “The thruster with anode layer (TAL) offers a narrow acceleration region [80, 82, 115]: a guard ring at the cathode potential is placed at the channel entrance to better localize the electric field.”
• Development and characterization of high -efficiency, high -specific impulse xenon Hall thrusters. (2004, background): “3 Wall effects and secondary electron emission The choice of wall material strongly influences the average electron temperature in the channel because of secondary electron emission (SEE) effects [151-153].”