Design and In-orbit Demonstration of REGULUS, an Iodine electric propulsion system

N Bellomo, M Magarotto, M Manente, F Trezzolani… - CEAS Space …, 2022 - Springer
REGULUS is an Iodine-based electric propulsion system. It has been designed and
manufactured at the Italian company Technology for Propulsion and Innovation SpA (T4i) …

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 …

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 …

Development of a novel wave plasma propulsion module with six-directional thrust vectoring capability

AI Shumeiko, VD Telekh, VI Mayorova - Acta Astronautica, 2022 - Elsevier
Nowadays, the development of low Earth orbits'(LEO)-up to 2000 km-small satellites (SSs) is
of particular interest. Such SSs are supposed to use for effective telecommunication systems …

Prediction of the Propulsive Performance of an Atmosphere-Breathing Electric Propulsion System on Cathode-Less Plasma Thruster

N Souhair, M Magarotto, R Andriulli, F Ponti - Aerospace, 2023 - mdpi.com
Atmosphere-breathing electric propulsion (ABEP) is a type of electric propulsion system that
uses the atmosphere as a propellant source instead of a stored reservoir. This technology is …

[HTML][HTML] Coupling of Fluid and Particle-in-Cell Simulations of Ambipolar Plasma Thrusters

W van Lynden, R Andriulli, N Souhair, F Ponti… - Aerospace, 2024 - mdpi.com
Ambipolar plasma thrusters are an appealing technology due to multiple system-related
advantages, including propellant flexibility and the absence of electrodes or neutralizer …

Development of a Global Model for the Analysis of Plasma in an Atmosphere-Breathing Cathode-Less Thruster

S Dalle Fabbriche, N Souhair, M Magarotto, R Andriulli… - Aerospace, 2023 - mdpi.com
This study investigates the preliminary propulsive performances of a cathode-less plasma
thruster with air as its propellant. The analysis is carried out through a global model and …

Zinc propellant storage and delivery system for hall thrusters

VG Tirila, A Hallock, A Demairé, CN Ryan - AIAA Propulsion and Energy …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-3407. vid Solid propellants are an
attractive alternative to xenon due to the generally larger storage densities, lower cost and …

Corrosion of metal parts on satellites by iodine exposure in space

D Zschätzsch, SL Benz, K Holste, M Vaupel… - Journal of Electric …, 2022 - Springer
Iodine becomes increasingly popular as alternative propellant for electric propulsion (EP)
systems offering several advantages over established xenon. However, iodine is also a …

[PDF][PDF] Improvement of a numerical tool for the simulation of a helicon plasma thruster

N Souhair, M Magarotto, M Manente… - Proceedings of the …, 2021 - researchgate.net
Recently, a numerical tool for the simulation of plasma production within discharge
chambers, namely 3DVIRTUS, was developed for the simulation of Helicon Plasma …