Electrodynamic Tether Systems on Small-Scale Spacecraft Using Dual-Purpose Materials for the Plasma-Spacecraft Interface-Reference-Cited by-同舟云学术

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Electrodynamic Tether Systems on Small-Scale Spacecraft Using Dual-Purpose Materials for the Plasma-Spacecraft Interface

Published:2013-09-10 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2013 Conference and Exposition
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Author:

McTernan Jesse K.¹,Bilen Sven G.¹

Affiliation:

1. Pennsylvania State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-5389

Reference18 articles.

1. 2Fuhrhop, K. "Theory and Experimental Evaluation of Electrodynamic Tether Systems and Related Technologies," Ph.D. Thesis,University of Michigan,2007.

2. 3Richardson,O.W.,TheEmissionofElectricityfromHotBodies,2nded.,Longmans,GreenandCo.,London,1921.

3. Fundamentals of Electric Propulasion

4. 5Domonkos, M. T. "Evaluation of Low-Current Orificed Hollow Cathodes," Ph.D. Thesis,The University of Michigan, 1999.

Cited by 1 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. Optimal Current Switch ing Control of Electrodynamic Tethers for Fast Deorbit;Journal of Guidance, Control, and Dynamics;2014-09

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