Simulations of plasma thruster effect on the electrostatic behavior of spacecrafts in GEO-Reference-Cited by-同舟云学术

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Simulations of plasma thruster effect on the electrostatic behavior of spacecrafts in GEO

Published:2015-08-28 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2015 Conference and Exposition
language:
Short-container-title:

Author:

Sarrailh Pierre¹,Hess Sebastien L.¹,Mateo-Velez Jean-Charles¹

Affiliation:

1. ONERA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-4640

Reference24 articles.

1. Performance and Evolution of Stationary Plasma Thruster Electric Propulsion for Large Communications Satellites

2. Masselin,M."DevelopmentofahybridPICcodeforthesimulationofplasmaspacecraftinteractions,"KTH,2012.

3. Reissner, A., Hummel, S., and Gengembre, E. "Development Status and Future of the European Electric Propulsion Plume Database,"2013.

Cited by 4 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. Modeling of a retarding potential analyzer and comparison with Express-A in-flight measurements;Frontiers in Physics;2022-10-07

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

3. Influence of secondary electron emission on plasma-surface interactions in the low earth orbit environment;Plasma Sources Science and Technology;2021-03-01

4. Kinetic Modeling of Spacecraft Surfaces in a Plume Backflow Region;IEEE Transactions on Plasma Science;2020-12

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