Electrostatic Analysis of an Artificial Orbiting Satellite for Absolute Charging
Author:
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Condensed Matter Physics,Nuclear and High Energy Physics
Link
http://xplorestaging.ieee.org/ielx7/27/7247791/07175062.pdf?arnumber=7175062
Cited by 7 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. Analysis of Differential Spacecraft Charging Using Suprathermal GEO Plasma Particles;2023 IEEE Microwaves, Antennas, and Propagation Conference (MAPCON);2023-12-11
2. A comparative study of body potential transient profile of geosynchronous orbit spacecraft in single and double Maxwellian plasma models;International Journal of Numerical Modelling: Electronic Networks, Devices and Fields;2021-10-19
3. Secondary and Backscattered Electron Current Induced Differential Charging on a Triple Junction of Spacecraft;IEEE Transactions on Plasma Science;2020-04
4. Impact of secondary and backscattered electron currents on absolute charging of structures used in spacecraft;International Journal of Numerical Modelling: Electronic Networks, Devices and Fields;2019-07-03
5. Heterogeneous Surface Multisphere Models Using Method of Moments Foundations;Journal of Spacecraft and Rockets;2019-07
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