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.
Full text not available from this repository.
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)|
|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
|Date Deposited:||15 Feb 2010|
|Last Modified:||31 Mar 2016 13:04|
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
Actions (login required)