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
1981 ◽  
Vol 18 (5) ◽  
pp. 457-461 ◽  
Author(s):  
M.R. Carruth ◽  
M.E. Brady

2010 ◽  
Vol 12 (2) ◽  
pp. 240-247 ◽  
Author(s):  
Sun Anbang ◽  
Mao Genwang ◽  
Yang Juan ◽  
Xia Guangqing ◽  
Chen Maolin ◽  
...  

2007 ◽  
Vol 15 (2) ◽  
pp. 83-94 ◽  
Author(s):  
Joseph Wang ◽  
Yong Cao ◽  
Raed Kafafy ◽  
Viktor Decyk

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%


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