An Open-Boundary Fully Kinetic PIC Model with Application to a Magnetically Enhanced Plasma Thruster

Shaun Andrews

University of Padova

Italy

3D full PIC simulation of the plume of a Magnetically Enhanced Plasma Thruster

Simone Di Fede

University of Padova

Italy

REGULUS: Iodine Fed Electric propulsion system for Small Satellites

Marco Minute

University of Padova

Italy

Analysis of different fluid approaches in the simulation of the source of a Helicon Plasma Thruster

Nabil Souhair

University of Bologna

Italy

Particle-In-Cell Simulation of Heavy Species in Hall Effect Thruster Plasma

Antonio Petronelli

Politecnico di Torino

Italy

Modified Two-Stream Instability in the E × B discharges of Hall thrusters

Federico Petronio

LPP

France

Spatially resolved Langmuir probe measurements in a non magnetized iodine ICP thruster

Benjamin Esteves

LPP

France

A multi-scale analysis of 2D PIC simulation of Hall Effect Thrusters using a collective Thomson scattering approach

Tarek Ben Slimane

LPP

France

Performance characterization and comparison with in-orbit results of a miniaturized gridded ion thruster using iodine

Lui Habl

LPP - ThrustMe

France

Multiscale modeling of a Hall thruster plume and comparison with Express-A in-flight measurements

Lucas Nicolle

ONERA

France

HPET-1: A Heated Electrospray Concept

Szymon Dworski

University of Southampton

England

The investigation of alternative solid propellants in Hall Thrusters

Vlad-George Tirila

University of Southampton

England