Jet extraction and characterization in an inertial electrostatic confinement device

@article{Chan2019JetEA,
  title={Jet extraction and characterization in an inertial electrostatic confinement device},
  author={Y.-A. Chan and Georg H. Herdrich},
  journal={Vacuum},
  year={2019}
}
Back-vacuum Retarding Potential Analyzer for Investigation of Plasma Properties from Inertial Electrostatic Confinement Thruster
A prototype of a back-vacuum retarding potential analyzer (RPA) is proposed, developed and set-up to resolve a known issue occurring in the conventional RPA measurement: particle accumulation. In
Influence of Cathode Dimension on Discharge Characteristics of Inertial Electrostatic Confinement Thruster
The concept of electric propulsion based on inertial electrostatic confinement (IEC) was proposed in 2017 IEPC accompanying with new theory explains the formation of its unique non-neutral plasma,
Breakthrough of Inertial Electrostatic Confinement Concept for Advanced Space Propulsion
The activities of Inertial electrostatic confinement (IEC) research for propulsion application in IRS started from 2009. A breakthrough on the theoretical explanation of working principle in 2017

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