Electrodeless plasma thrusters for spacecraft: a review
SN Bathgate, MMM Bilek… - Plasma Science and …, 2017 - iopscience.iop.org
The physics of electrodeless electric thrusters that use directed plasma to propel spacecraft
without employing electrodes subject to plasma erosion is reviewed. Electrodeless plasma …
without employing electrodes subject to plasma erosion is reviewed. Electrodeless plasma …
The 2017 Plasma Roadmap: Low temperature plasma science and technology
Abstract Journal of Physics D: Applied Physics published the first Plasma Roadmap in 2012
consisting of the individual perspectives of 16 leading experts in the various sub-fields of low …
consisting of the individual perspectives of 16 leading experts in the various sub-fields of low …
[HTML][HTML] Perspectives, frontiers, and new horizons for plasma-based space electric propulsion
There are a number of pressing problems mankind is facing today that could, at least in part,
be resolved by space systems. These include capabilities for fast and far-reaching …
be resolved by space systems. These include capabilities for fast and far-reaching …
Ion thrusters for electric propulsion: Scientific issues developing a niche technology into a game changer
K Holste, P Dietz, S Scharmann, K Keil… - Review of Scientific …, 2020 - pubs.aip.org
The transition from old space to new space along with increasing commercialization has a
major impact on space flight, in general, and on electric propulsion (EP) by ion thrusters, in …
major impact on space flight, in general, and on electric propulsion (EP) by ion thrusters, in …
Neutral gas depletion in low temperature plasma
A Fruchtman - Journal of Physics D: Applied Physics, 2017 - iopscience.iop.org
Neutral depletion can significantly affect the steady state of low temperature plasmas.
Processes that lead to neutral depletion and the resulting plasma–neutrals steady state are …
Processes that lead to neutral depletion and the resulting plasma–neutrals steady state are …
Integrated study on the comprehensive magnetic-field configuration performance in the 150 kW superconducting magnetoplasmadynamic thruster
J Zheng, H Liu, Y Song, C Zhou, Y Li, M Li, H Tang… - Scientific Reports, 2021 - nature.com
Higher magnetic fields are always favoured in the magnetoplasmadynamic thruster (MPDT)
due to its superior control of the plasma profile and acceleration process. This paper …
due to its superior control of the plasma profile and acceleration process. This paper …
Radio-frequency biasing of ion acceleration grids with different propellants
In order to ensure the space charge compensation of the plume, conventional ion thrusters
need an additional neutralizer to release electrons. When a radio-frequency (RF) voltage is …
need an additional neutralizer to release electrons. When a radio-frequency (RF) voltage is …
A numerical investigation on electron runaway threshold at the initial stage of atmospheric streamer development
M Jiang, L Zou, J Zhang, H Wang, Y Li, C Liu… - Physics of …, 2023 - pubs.aip.org
Pre-ionization caused by runaway electrons is an important mechanism for negative
streamer development. The aim of this paper is to investigate the runaway criteria and …
streamer development. The aim of this paper is to investigate the runaway criteria and …
Plasma plume expansion with pulsed electron neutralization
Electrons neutralizing the ion beam from a gridded ion source are typically provided by an
external cathode. This cathode emits a continuous current that ensures quasi-neutrality of …
external cathode. This cathode emits a continuous current that ensures quasi-neutrality of …
Effects of water-vapor propellant on electrodeless thruster performance
EM Petro, RJ Sedwick - Journal of Propulsion and Power, 2017 - arc.aiaa.org
The performance of an electrodeless thruster operating on water-vapor propellant is
evaluated and compared to noble-gas propellants. Cross-section data for electron …
evaluated and compared to noble-gas propellants. Cross-section data for electron …