The effect of alternative propellants on the electron drift instability in Hall-effect thrusters: Insight from 2D particle-in-cell simulations-Reference-Cited by-同舟云学术

The effect of alternative propellants on the electron drift instability in Hall-effect thrusters: Insight from 2D particle-in-cell simulations

Author:

Croes Vivien¹²,Tavant Antoine¹²^ORCID,Lucken Romain¹,Martorelli Roberto¹,Lafleur Trevor³,Bourdon Anne¹^ORCID,Chabert Pascal¹

Affiliation:

1. Laboratoire de Physique des Plasmas, CNRS, Sorbonne Université, Université Paris Sud, École Polytechnique, F-91120 Palaiseau, France

2. Safran Aircraft Engines, Electric Propulsion Unit, F-27208 Vernon, France

3. PlasmaPotential—Physics Consulting and Research, Canberra ACT 2601, Australia

Funder

Agence Nationale de la Recherche

Horizon 2020 Framework Programme

Grand Équipement National De Calcul Intensif

Publisher

AIP Publishing

Subject

Condensed Matter Physics

Link

Reference56 articles.

1. R. Villain , “Satellites to be built and launched by 2014,” Euroconsult Research Report No. 8 (2005).

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