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 …

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 …

[HTML][HTML] Physics of E× B discharges relevant to plasma propulsion and similar technologies

ID Kaganovich, A Smolyakov, Y Raitses, E Ahedo… - Physics of …, 2020 - pubs.aip.org
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 …

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 …

Electron diamagnetic effect on axial force in an expanding plasma: experiments and theory

K Takahashi, T Lafleur, C Charles, P Alexander… - Physical review …, 2011 - APS
The axial force imparted from a magnetically expanding current-free plasma is directly
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

K Takahashi, C Charles, RW Boswell - Physical review letters, 2013 - APS
Cross-field diffusion and plasma expansion in a rapidly diverging magnetic nozzle are
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 …

Helicon thruster plasma modeling: Two-dimensional fluid-dynamics and propulsive performances

E Ahedo, J Navarro-Cavallé - Physics of Plasmas, 2013 - pubs.aip.org
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 …

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 …

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 …