Kinetic electron model for plasma thruster plumes

e-Archivo Repository

Show simple item record

dc.contributor.author Merino Martínez, Mario
dc.contributor.author Maurino, Javier
dc.contributor.author Ahedo Galilea, Eduardo Antonio
dc.date.accessioned 2019-06-18T10:52:19Z
dc.date.available 2019-06-18T10:52:19Z
dc.date.issued 2018-03-28
dc.identifier.bibliographicCitation Merino, M., Mauriño, J. y Ahedo E. (2018). Kinetic electron model for plasma thruster plumes. Plasma Sources Science and Technology, 27(3).
dc.identifier.issn 0963-0252
dc.identifier.uri http://hdl.handle.net/10016/28508
dc.description.abstract A paraxial model of an unmagnetized, collisionless plasma plume expanding into vacuum is presented. Electrons are treated kinetically, relying on the adiabatic invariance of their radial action integral for the integration of Vlasov's equation, whereas ions are treated as a cold species. The quasi-2D plasma density, self-consistent electric potential, and electron pressure, temperature, and heat fluxes are analyzed. In particular, the model yields the collisionless cooling of electrons, which differs from the Boltzmann relation and the simple polytropic laws usually employed in fluid and hybrid PIC/fluid plume codes.
dc.description.sponsorship The authors want to thank Professor Jesús Ramos from the Massachusetts Institute of Technology, and Dr Jaume Navarro, Dr Gonzalo Sánchez-Arriaga, and Dr Pablo Fajardo from Universidad Carlos III de Madrid for many insightful discussions and comments.This work has been supported by ESA project 4000116180/15/NL/PS. The work of Javier Mauriño has been supported by the UK Royal Academy of Engineering's Engineering Leaders Scholarship (ELAA1516/1/87).
dc.format.extent 21
dc.language.iso eng
dc.publisher IOP Publishing
dc.rights © 2018 IOP Publishing Ltd.
dc.subject.other Electric propulsion
dc.subject.other Plasma thrusters
dc.subject.other Plasma plumes
dc.subject.other Kinetic models
dc.subject.other Collisionless plasma
dc.subject.other Electron cooling
dc.title Kinetic electron model for plasma thruster plumes
dc.type article
dc.subject.eciencia Aeronáutica
dc.identifier.doi https://doi.org/10.1088/1361-6595/aab3a1
dc.rights.accessRights openAccess
dc.type.version acceptedVersion
dc.identifier.publicationissue 3
dc.identifier.publicationtitle Plasma Sources Science & Technology
dc.identifier.publicationvolume 27
dc.identifier.uxxi AR/0000021315
 Find Full text

Files in this item

*Click on file's image for preview. (Embargoed files's preview is not supported)


This item appears in the following Collection(s)

Show simple item record