Three dimensional PIC-DSMC simulations of Hall thruster plumes and analysis for realistic spacecraft configurations-Reference-Cited by-同舟云学术

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Three dimensional PIC-DSMC simulations of Hall thruster plumes and analysis for realistic spacecraft configurations

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Oh David¹,Hastings Daniel¹

Affiliation:

1. MIT, Cambridge, MA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3299

Reference17 articles.

1. Emissions,"EEPC Paper 93-097,September 1993.

2. 2Arkhipov,B.A.andKozubsky,K.N. "TheDevelopment of the Cathodes-Compensators for Stationary Plasma Thrusters inUSSR,"ffiPC Paper 91-023, October 1991.

3. Hall thruster ion beam characterization

4. Numerical simulation of stationary plasma thruster exhaust plume

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Quantifying Uncertainty in Predictions of Spacecraft Erosion Induced by a Hall Thruster;Journal of Spacecraft and Rockets;2021-12-22

2. Comparison of Hall Thruster Plume Expansion Model with Experimental Data;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

3. Particle-in-Cell with Monte Carlo Simulation of SPT-100 Exhaust Plumes;Journal of Spacecraft and Rockets;2002-05

4. Impact Analysis of Hall Thrusters on Satellite Antenna Performance;Journal of Spacecraft and Rockets;2002-01

5. Particle Simulations of a Hall Thruster Plume;Journal of Spacecraft and Rockets;2000-01

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