Feasibility of MEMS hollow cathode devices for micro-spacecraft plasma propulsion
Grubisic, Angelo N., Cranny, Andy and Gabriel, Stephen B. (2008) Feasibility of MEMS hollow cathode devices for micro-spacecraft plasma propulsion. In, 14th International Congress on Plasma Physics, Fukuoka, Japan, 08 - 12 Sep 2008. 11pp.
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Original Publication URL: http://www.triam.kyushu-u.ac.jp/ICPP/program/downl...
Description/Abstract
Micro-satellites in the 1-20kg range with limited onboard resources would benefit greatly from miniaturized, low power electric propulsion systems. This paper reports on a feasibility study into the scaling and application of MEMS manufacturing techniques to produce such a micro-hollow cathode thruster
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Related URLs: | |
| Keywords: | MEMS, hollow cathode thruster plasma, propulsion |
| Subjects: | U Military Science > U Military Science (General) T Technology > TL Motor vehicles. Aeronautics. Astronautics Q Science > QC Physics |
| Divisions: | University Structure - Pre August 2011 > School of Engineering Sciences > Astronautics |
| Item ID: | 72467 |
| Date Deposited: | 15 Feb 2010 |
| Last Modified: | 02 Mar 2012 12:53 |
| Contributors: | Grubisic, Angelo N. (Author) Cranny, Andy (Author) Gabriel, Stephen B. (Author) |
| Date: | 7 September 2008 |
| Status: | Published |
| URI: | http://eprints.soton.ac.uk/id/eprint/72467 |
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