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 …

Fully kinetic model of plasma expansion in a magnetic nozzle

S Andrews, S Di Fede… - Plasma Sources Science …, 2022 - iopscience.iop.org
A self-consistent model is presented for performing steady-state fully kinetic particle-in-cell
simulations of magnetised plasma plumes. An energy-based electron reflection prevents the …

Development of a counterbalanced pendulum thrust stand for electric propulsion

F Trezzolani, M Magarotto, M Manente, D Pavarin - Measurement, 2018 - Elsevier
We have designed and tested a thrust stand for RF plasma thrusters characterization. The
balance is employed in the development of small and medium size RF plasma thrusters; it …

Simulation of the plume of a magnetically enhanced plasma thruster with SPIS

S Di Fede, M Magarotto, S Andrews… - Journal of Plasma …, 2021 - cambridge.org
A three-dimensional fully kinetic particle-in-cell (PIC) simulation strategy has been
implemented to simulate the acceleration stage of a magnetically enhanced plasma thruster …

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 …

Fully magnetized plasma flow in a magnetic nozzle

M Merino, E Ahedo - Physics of Plasmas, 2016 - pubs.aip.org
A model of the expansion of a plasma in a magnetic nozzle in the full magnetization limit is
presented. The fully magnetized and the unmagnetized-ions limits are compared, recovering …

Results of the first Helicon Plasma Thruster (HPT) coupling test campaign within the HIPATIA project

M Ruiz, A Velasco, V Gómez… - 37th International …, 2022 - hal.science
HIPATIA (HelIcon PlasmA Thruster for In-Space Applications) project was awarded with a
European Commission H2020 grant for the development of the HPT (Helicon Plasma …

Development and Testing of a Helicon Plasma Thruster Based on a Magnetically Enhanced Inductively Coupled Plasma Reactor Operating in a Multi-Mode Regime.

AMT Andreescu, DE Crunteanu… - Applied Sciences …, 2024 - search.ebscohost.com
A disruptive Electric Propulsion system is proposed for next-generation Low-Earth-Orbit
(LEO) small satellite constellations, utilizing an RF-powered Helicon Plasma Thruster (HPT) …

[PDF][PDF] Maiden tests of the HPT05 helicon plasma thruster prototype

M Merino, J Navarro, E Ahedo, V Gómez… - … et Astronautique de …, 2016 - ep2.uc3m.es
A flexible 1 kW helicon plasma thruster prototype called HTP05 has been designed and built
by SENER and EP2, with the aim of improving the present understanding of the physical …