An intense Hall-type ion source for satellite propulsion
Author:
Publisher
AIP Publishing
Subject
Instrumentation
Link
http://aip.scitation.org/doi/pdf/10.1063/1.1148572
Reference2 articles.
1. Investigation of a small, closed electron drift, stationary plasma thruster
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3. Effects of initial ion velocity, magnetic field and plasma density profiles in simulating the plasma plume in a Hall thruster;Journal of Astrophysics and Astronomy;2023-01-16
4. Electron energy distribution function in a low-power Hall thruster discharge and near-field plume;Physics of Plasmas;2018-06
5. Emission-Excitation Cross Sections Relevant to Krypton-Propelled Electric Thrusters;Journal of Propulsion and Power;2015-03
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