scholarly journals Gas inlet impact on neutral density and recycle pattern with a disk shaped antenna in a miniature ion thruster through particle simulation

AIP Advances ◽  
2021 ◽  
Vol 11 (12) ◽  
pp. 125209
Author(s):  
Ali Yousefian
Keyword(s):  
Particle Simulation ◽  
Neutral Density ◽  
Ion Thruster

Particle simulation of charge-exchange ions back flow in ion thruster plume

2011 ◽  
Vol 23 (7) ◽  
pp. 1929-1934
Author(s):  
任军学 Ren Junxue ◽  
李娟 Li Juan ◽  
仇钎 Qiu Qian ◽  
汤海滨 Tang Haibin ◽  
温正 Wen Zheng
Keyword(s):  
Charge Exchange ◽  
Particle Simulation ◽  
Back Flow ◽  
Ion Thruster

Particle Simulation of Three-Grid ECR Ion Thruster Optics and Erosion Prediction

2010 ◽  
Vol 12 (2) ◽  
pp. 240-247 ◽  
Author(s):  
Sun Anbang ◽  
Mao Genwang ◽  
Yang Juan ◽  
Xia Guangqing ◽  
Chen Maolin ◽  
...  
Keyword(s):  
Particle Simulation ◽  
Ion Thruster ◽  
Erosion Prediction

scholarly journals Electric Propulsion Plume Simulations Using Parallel Computer

2007 ◽  
Vol 15 (2) ◽  
pp. 83-94 ◽  
Author(s):  
Joseph Wang ◽  
Yong Cao ◽  
Raed Kafafy ◽  
Viktor Decyk
Keyword(s):  
Electric Propulsion ◽  
Large Scale ◽  
Three Dimensional ◽  
Particle Simulation ◽  
Parallel Computer ◽  
Solar Array ◽  
Electron Mass ◽  
Ion Thruster ◽  
Particle In Cell ◽  
Pic Code

A parallel, three-dimensional electrostatic PIC code is developed for large-scale electric propulsion simulations using parallel supercomputers. This code uses a newly developed immersed-finite-element particle-in-cell (IFE-PIC) algorithm designed to handle complex boundary conditions accurately while maintaining the computational speed of the standard PIC code. Domain decomposition is used in both field solve and particle push to divide the computation among processors. Two simulations studies are presented to demonstrate the capability of the code. The first is a full particle simulation of near-thruster plume using real ion to electron mass ratio. The second is a high-resolution simulation of multiple ion thruster plume interactions for a realistic spacecraft using a domain enclosing the entire solar array panel. Performance benchmarks show that the IFE-PIC achieves a high parallel efficiency of ≥ 90%

Three-dimensional particle simulation of ion thruster plume flows with EX-PWS

2018 ◽  
Vol 20 (10) ◽  
pp. 105501 ◽  
Author(s):  
Hongru ZHENG ◽  
Guobiao CAI ◽  
Hongyue WANG ◽  
Lihui LIU ◽  
Bijiao HE
Keyword(s):  
Three Dimensional ◽  
Particle Simulation ◽  
Ion Thruster ◽  
Plume Flows

Estimate of Lifetime of Ion Thruster Optics Based on Particle Simulation

2008 ◽  
Vol 10 (1) ◽  
pp. 46-52 ◽  
Author(s):  
Liu Chang ◽  
Tang Haibin ◽  
Zhang Zhenpeng ◽  
Gu Zuo ◽  
Liu Yu
Keyword(s):  
Particle Simulation ◽  
Ion Thruster

Particle simulation of ion thruster plume characteristics

2010 ◽  
Vol 22 (2) ◽  
pp. 401-405
Author(s):  
孙安邦 Sun Anbang ◽  
毛根旺 Mao Genwang ◽  
陈茂林 Chen Maolin ◽  
夏广庆 Xia Guangqing ◽  
霍超 Huo Chao
Keyword(s):  
Particle Simulation ◽  
Ion Thruster

Particle simulation of ion thruster using parallel computation on graphic processor unit

2011 ◽  
Vol 23 (2) ◽  
pp. 507-511
Author(s):  
仇钎 Qiu Qian ◽  
刘宇 Liu Yu ◽  
任军学 Ren Junxue ◽  
汤海滨 Tang Haibin ◽  
钟凌伟 Zhong Lingwei ◽  
...  
Keyword(s):  
Parallel Computation ◽  
Particle Simulation ◽  
Graphic Processor Unit ◽  
Ion Thruster ◽  
Graphic Processor ◽  
Processor Unit
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