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Electric propulsion for satellites and spacecraft: established technologies and novel approaches
S Mazouffre - Plasma Sources Science and Technology, 2016 - iopscience.iop.org
This contribution presents a short review of electric propulsion (EP) technologies for
satellites and spacecraft. Electric thrusters, also termed ion or plasma thrusters, deliver a low …
satellites and spacecraft. Electric thrusters, also termed ion or plasma thrusters, deliver a low …
Helicon-type radiofrequency plasma thrusters and magnetic plasma nozzles
K Takahashi - Reviews of Modern Plasma Physics, 2019 - Springer
Abstract Development of electrodeless radiofrequency plasma thrusters, eg, a helicon
thruster, has been one the of challenging topics for future high-power and long-lived electric …
thruster, has been one the of challenging topics for future high-power and long-lived electric …
[HTML][HTML] Physics of E× B discharges relevant to plasma propulsion and similar technologies
This paper provides perspectives on recent progress in understanding the physics of
devices in which the external magnetic field is applied perpendicular to the discharge …
devices in which the external magnetic field is applied perpendicular to the discharge …
Plasmas for space propulsion
E Ahedo - Plasma Physics and Controlled Fusion, 2011 - iopscience.iop.org
Plasma thrusters are challenging the monopoly of chemical thrusters in space propulsion.
The specific energy that can be deposited into a plasma beam is orders of magnitude larger …
The specific energy that can be deposited into a plasma beam is orders of magnitude larger …
Electron diamagnetic effect on axial force in an expanding plasma: experiments and theory
The axial force imparted from a magnetically expanding current-free plasma is directly
measured for three different experimental configurations and compared with a two …
measured for three different experimental configurations and compared with a two …
Approaching the Theoretical Limit of Diamagnetic-Induced Momentum<? format?> in a Rapidly Diverging Magnetic Nozzle
Cross-field diffusion and plasma expansion in a rapidly diverging magnetic nozzle are
controlled while maintaining constant plasma production in a contiguously attached radio …
controlled while maintaining constant plasma production in a contiguously attached radio …
Helicon plasma thruster discharge model
T Lafleur - Physics of Plasmas, 2014 - pubs.aip.org
By considering particle, momentum, and energy balance equations, we develop a semi-
empirical quasi one-dimensional analytical discharge model of radio-frequency and helicon …
empirical quasi one-dimensional analytical discharge model of radio-frequency and helicon …
Helicon thruster plasma modeling: Two-dimensional fluid-dynamics and propulsive performances
An axisymmetric macroscopic model of the magnetized plasma flow inside the helicon
thruster chamber is derived, assuming that the power absorbed from the helicon antenna …
thruster chamber is derived, assuming that the power absorbed from the helicon antenna …
Plasma beam characterization along the magnetic nozzle of an ECR thruster
S Correyero, J Jarrige, D Packan… - … Sources Science and …, 2019 - iopscience.iop.org
Experimental characterization of plasma properties along the magnetic nozzle of an electron
cyclotron resonance thruster is presented here. A permanent magnet (PM) prototype and a …
cyclotron resonance thruster is presented here. A permanent magnet (PM) prototype and a …
Direct thrust measurement of an electron cyclotron resonance plasma thruster
T Vialis, J Jarrige, A Aanesland… - Journal of Propulsion and …, 2018 - arc.aiaa.org
Direct thrust measurements of an electron cyclotron resonance plasma thruster are
performed with a thrust balance. The thruster performances are deduced, and the influence …
performed with a thrust balance. The thruster performances are deduced, and the influence …