Effects of the radial plasma-wall interaction on the Hall thruster discharge
By Eduardo Ahedo, J. Gallardo, M. Martínez-Sánchez. 2003
135 citations recorded by the source corpus.
Subfields: Atomic and Molecular Physics, and Optics, Electrical and Electronic Engineering
View Paper: https://www.semanticscholar.org/paper/c77fc7318e31f5de331a85391b6c7c093c8ca5b0
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In Atomic and Molecular Physics, and Optics
In Electrical and Electronic Engineering
Citations in the corpus
- The Influence of Neutral Flow Rate in the Operation of Hall Thrusters. (2009, methodology): “247 The electron-wall collision frequency was modeled as [18, 61, 163, 164]”
- Electric propulsion for satellites and spacecraft: established technologies and novel approaches (2016, background): “Evaluation of near-wall transport by means of numerical simulations indicates this mechanism is insufficient to explain the level of anomalous transverse electron diffusion [103, 104].”
- Physics of E × B discharges relevant to plasma propulsion and similar technologies (2020, unknown): “8,9,20,23 Moreover, the high-energy electrons that can escape to the walls with energy above the potential energy corresponding to the wall potential are not being replenished sufficiently fast.”