The effects of numerical acceleration techniques on PIC-MCC simulations of ion thrusters-Reference-Cited by-同舟云学术

The effects of numerical acceleration techniques on PIC-MCC simulations of ion thrusters

Published:2020-04-01 Issue:4 Volume:10 Page:045115
ISSN:2158-3226
Container-title:AIP Advances
language:en
Short-container-title:AIP Advances

Author:

Yuan Tiannan¹²^ORCID,Ren Junxue¹²,Zhou Jun¹²,Zhang Zhe²³^ORCID,Wang Yibai¹²,Tang Haibin²⁴

Affiliation:

1. School of Astronautics, Beihang University, Beijing 100191, People’s Republic of China

2. Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies of Ministry of Education, Beihang University, Beijing 100191, People’s Republic of China

3. School of Instrumentation and Optoelectronic Engineering, Beihang University, Beijing 100191, People’s Republic of China

4. School of Space and Environment, Beihang University, Beijing 100191, People’s Republic of China

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5113561

Reference51 articles.

1. Wall material effects in stationary plasma thrusters. II. Near-wall and in-wall conductivity

2. Magnetic shielding of the channel walls in a Hall plasma accelerator

3. K. Hara, “Development of grid-based direct kinetic method and hybrid kinetic-continuum modeling of Hall thruster discharge plasmas,” Ph.D. dissertation (University of Michigan, 2015).

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