Mr
Florian Marmuse
(LPP - UPMC)
3/2/17, 4:00 PM
Poster
Evaluating a thruster performances in a representative operational environment is a key milestone towards its use in space. However, the limited size and pumping speed of currently available test facilities limit the validity of most performance measurements, from the plume divergence to the thruster lifetime expectancy. Based on a literature review, this poster features a panel of the...
Dr
Grazia Cicala
(CNR-NANOTEC)
3/2/17, 4:00 PM
Poster
Neutralizer cathodes used as electron sources represent a key component of electric propulsion (EP) systems for spacecrafts. In EP systems such as electric propulsion thrusters, ion engines and hall thrusters, a positive ion beam is ejected at high speed to produce thrust. Over time, the ion beam expands and becomes fuzzy for the space charge formation that reduces the thrust and causes arcing...
Mr
Francesco Paolo Micchetti
(EnginSoft)
3/2/17, 4:00 PM
Poster
A software methodology implemented through an extremely user-friendly UI, able to simulate an Hall Effect Thruster, starting from its physical dimensions up to specific material and atomic species data, will be showcased.
Mr
Romain Lucken
(Laboratoire de physique des Plasmas)
3/2/17, 4:00 PM
Poster
R. Lucken, T. Lafleur, P. Grondein, A. Bourdon, P. Chabert, A. Aanesland
LPP, CNRS, Ecole polytechnique, UPMC Univ Paris 06, Univ. Paris-Sud, Observatoire de Paris, Université Paris-Saclay, Sorbonne Universitś, PSL Research University, 91128 Palaiseau, France
PEGASES is an ion-ion thruster concept developed at LPP for over ten years. The neutralization of the plume by alternate negative...
Marco Cavenago
(LNL)
3/2/17, 4:00 PM
Poster
Complex plasma devices as thrusters or ion sources for fusion and their physical models at reduced size, as the negative ion source NIO1 developed by Consorzio RFX and INFN-LNL, rely on several accessories, like coil shielding, cesium vaporizers, probes and bias electrodes, which needs to be separately tested , both to avoid delays in the major source schedule and to better understand...
Mr
Antoine Tavant
(LPP)
3/2/17, 4:00 PM
Poster
Hall effect thrusters (HET) are one of the main technology used and studies for spacecraft propulsion. Grid-less, they present net advantages, resulting of an increasing need for predictive and accurate models, and a better understanding of the complex behavior of the plasma.
HETs consist of three main components : a magnetic circuit used to produce a mostly radial magnetic field; an...
