The Innovative Dual-Stage 4-Grid Ion Thruster Concept - Theory And Experimental Results-Reference-Cited by-同舟云学术

The Innovative Dual-Stage 4-Grid Ion Thruster Concept - Theory And Experimental Results

Published:2006-10-02 Issue: Volume: Page:
ISSN:
Container-title:57th International Astronautical Congress
language:
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Author:

Bramanti Cristina¹,Walker Roger¹,Sutherland Orson²,Boswell Rod²,Charles Christine²,Fearn David³,Amo Jose Gonzalez Del¹,Orlandi Marika¹

Affiliation:

1. ESA-ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2. Plasma Research Laboratory, Research School of Physical Sciences and Engineering, The Australian National University, Canberra, ACT 0200, Australia

3. EP Solutions, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.IAC-06-C4.4.07

Reference12 articles.

1. High power beams for neutral injection heating

2. Quasi–dc extraction of 70 keV, 5 A ion beam

3. Power transmission characteristics of a two‐stage multiaperture neutral beam source

4. Numerical simulation for design of a two‐stage acceleration system in a megawatt power ion source

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