[HTML][HTML] Far-field plume characterization of a low-power cylindrical Hall thruster

T Perrotin, AE Vinci, S Mazouffre, P Fajardo… - Journal of Applied …, 2024 - pubs.aip.org
A fully cylindrical Hall thruster prototype was tested in the power range of 30–300 W with the
objective of understanding the behavior of the discharge as a function of input parameters …

[PDF][PDF] Direct thrust measurements of a 200 W Cylindrical Hall Thruster

T Perrotin, P Fajardo, J Navarro-Cavallé… - … , IEPC-2024-747 …, 2024 - ep2.uc3m.es
A fully Cylindrical Hall Thruster is tested in the 200-400 W range of discharge power,
coupled to a sub-ampere hollow cathode in self-sustained mode. The operating envelope …