Multi-GPU PIC solver for modeling of ion thruster plasma plume

Revathi Jambunathan, Deborah A. Levin

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Three-dimensional particle-in-cell simulations are performed to study the characteristics of xenon mesothermal plasma plumes and their interaction with the neutralizer electrons. To study the effect of electron source location on the plume dynamics and electron kinetics, two configurations are modeled, one with co-located electron and ion sources and the second with a shifted electron source. In addition, the effect of electrostatic boundary condition on the plume dynamics of the shifted electron case are also studied by implementing a fixed Dirichlet boundary condition of φ =0 V at all the boundaries. In the first case, the plume achieved a quasi-neutral state by the electrostatic trapping of electrons within the confined xenon ion plume. For the shifted electron source, however, no such symmetry was observed and the electrons are found to oscillate, resulting in counterstreaming electron populations. Compared to the Neumann boundary condition, the case with the Dirichlet boundary condition was found to affect the electron velocities as the beam-front approached closer to the boundary, consequently affecting the plume dynamics.

Original languageEnglish (US)
Title of host publicationAIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Edition210059
ISBN (Print)9781624105241
DOIs
StatePublished - Jan 1 2018
EventAIAA Aerospace Sciences Meeting, 2018 - Kissimmee, United States
Duration: Jan 8 2018Jan 12 2018

Publication series

NameAIAA Aerospace Sciences Meeting, 2018
Number210059

Other

OtherAIAA Aerospace Sciences Meeting, 2018
CountryUnited States
CityKissimmee
Period1/8/181/12/18

Fingerprint

Electron sources
Plasmas
Electrons
Ions
Boundary conditions
Xenon
Electrostatics
Beam plasma interactions
Ion sources
Graphics processing unit
Kinetics

ASJC Scopus subject areas

  • Aerospace Engineering

Cite this

Jambunathan, R., & Levin, D. A. (2018). Multi-GPU PIC solver for modeling of ion thruster plasma plume. In AIAA Aerospace Sciences Meeting (210059 ed.). (AIAA Aerospace Sciences Meeting, 2018; No. 210059). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2018-1297

Multi-GPU PIC solver for modeling of ion thruster plasma plume. / Jambunathan, Revathi; Levin, Deborah A.

AIAA Aerospace Sciences Meeting. 210059. ed. American Institute of Aeronautics and Astronautics Inc, AIAA, 2018. (AIAA Aerospace Sciences Meeting, 2018; No. 210059).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Jambunathan, R & Levin, DA 2018, Multi-GPU PIC solver for modeling of ion thruster plasma plume. in AIAA Aerospace Sciences Meeting. 210059 edn, AIAA Aerospace Sciences Meeting, 2018, no. 210059, American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA Aerospace Sciences Meeting, 2018, Kissimmee, United States, 1/8/18. https://doi.org/10.2514/6.2018-1297
Jambunathan R, Levin DA. Multi-GPU PIC solver for modeling of ion thruster plasma plume. In AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA. 2018. (AIAA Aerospace Sciences Meeting, 2018; 210059). https://doi.org/10.2514/6.2018-1297
Jambunathan, Revathi ; Levin, Deborah A. / Multi-GPU PIC solver for modeling of ion thruster plasma plume. AIAA Aerospace Sciences Meeting. 210059. ed. American Institute of Aeronautics and Astronautics Inc, AIAA, 2018. (AIAA Aerospace Sciences Meeting, 2018; 210059).
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