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 …

Thirty percent conversion efficiency from radiofrequency power to thrust energy in a magnetic nozzle plasma thruster

K Takahashi - Scientific reports, 2022 - nature.com
Innovations for terrestrial transportation technologies, eg, cars, aircraft, and so on, have
driven historical industries so far, and a similar breakthrough is now occurring in space …

REGULUS: A propulsion platform to boost small satellite missions

M Manente, F Trezzolani, M Magarotto, E Fantino… - Acta Astronautica, 2019 - Elsevier
REGULUS is a propulsion platform for CubeSats. It integrates the Magnetically Enhanced
Thruster (MET) and its subsystems (ie, fluidic line, electronics, and thermo-structural …

Development of a lumping methodology for the analysis of the excited states in plasma discharges operated with argon, neon, krypton, and xenon

N Souhair, M Magarotto, E Majorana, F Ponti… - Physics of …, 2021 - pubs.aip.org
In this paper, a methodology is presented to compute the plasma properties (eg,, density
and temperature) accounting for the dynamics of the excited states. The proposed strategy …

Numerical model of a helicon plasma thruster

M Magarotto, M Manente, F Trezzolani… - IEEE Transactions on …, 2020 - ieeexplore.ieee.org
This article is devoted to the presentation of a numerical model of a Helicon Plasma Thruster
(HPT) which relies on: 1) the 3-D adVanced fluId dRifT diffUsion plaSma solver (3D …

Parametric study of a cathode-less radio frequency thruster

M Magarotto, D Pavarin - IEEE Transactions on Plasma …, 2020 - ieeexplore.ieee.org
A cathode-less radio frequency (RF) thruster is a plasma-based system for space
propulsion. It consists on a source for plasma generation driven by an RF antenna and a …

Semi-analytical model of a helicon plasma thruster

M Guaita, M Magarotto, M Manente… - … on Plasma Science, 2022 - ieeexplore.ieee.org
This article is devoted to the presentation of a semianalytical model of a helicon plasma
thruster based on: 1) a 0-D global source model (GSM) for the simulation of the plasma …

[HTML][HTML] Analysis of the plasma transport in numerical simulations of helicon plasma thrusters

N Souhair, M Magarotto, F Ponti, D Pavarin - AIP Advances, 2021 - pubs.aip.org
The accurate simulation of the plasma transport in helicon sources is a key aspect to
improve the design of Helicon Plasma Thrusters (HPTs). Specifically, the 3D-VIRTUS code …

Study on the influence of the magnetic field geometry on the power deposition in a helicon plasma source

M Magarotto, D Melazzi, D Pavarin - Journal of Plasma Physics, 2019 - cambridge.org
We have numerically studied how an actual confinement magnetostatic field affects power
deposition in a helicon source. We have solved the wave propagation by means of two …

[PDF][PDF] Diagnostic methods for the characterization of a helicon plasma thruster

M Wijnen - 2023 - core.ac.uk
This thesis is dedicated to the development of several diagnostics for the characterization of
electric propulsion devices in general and of RF and helicon plasma thrusters in particular …