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 …

The 2017 Plasma Roadmap: Low temperature plasma science and technology

I Adamovich, SD Baalrud, A Bogaerts… - Journal of Physics D …, 2017 - iopscience.iop.org
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 …

[HTML][HTML] Perspectives, frontiers, and new horizons for plasma-based space electric propulsion

I Levchenko, S Xu, S Mazouffre, D Lev, D Pedrini… - Physics of …, 2020 - pubs.aip.org
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 …

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 …

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 …

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 …

Radio-frequency biasing of ion acceleration grids with different propellants

Y Li, H Tang, G Cai, C Fu, W Wang - Plasma Sources Science …, 2022 - iopscience.iop.org
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 …

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 …

Plasma plume expansion with pulsed electron neutralization

L Habl, T Lafleur, D Rafalskyi… - Plasma Sources Science …, 2021 - iopscience.iop.org
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 …

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 …