Design and installation of a field ionization test chamber for ion thrusters
dc.contributor.advisor | Osswald, Sebastian | |
dc.contributor.advisor | Romano, Marcello | |
dc.contributor.author | Camp, Paul W. | |
dc.date | December 2011 | |
dc.date.accessioned | 2012-08-22T15:32:50Z | |
dc.date.available | 2012-08-22T15:32:50Z | |
dc.date.issued | 2011-12 | |
dc.identifier.uri | https://hdl.handle.net/10945/10574 | |
dc.description.abstract | The utilization of carbon nanotube arrays for field ionization in ion thrusters allows for a substantial reduction in thruster size and weight. The availability of miniature ion thrusters may enable the development of a suitable propulsion system for nano- and picosatellites, and can realize substantial weight, volume, and cost savings in existing satellite platforms. This research focuses on the design of a field ionization test chamber that can be used to determine a comprehensive performance metric for the carbon nanotube field ionization micro-ion thruster (CNTFIMIT). Using the knowledge gathered from two previously employed test chamber designs, a third generation apparatus with higher precision and improved capabilities is constructed. This new design incorporates a mass flow controller for propellant flow rate measurements, a high-voltage source-measure unit for ionization current measurements, and a linear shift with position feedback for adjusting the distance between the carbon nanotubes and the counter electrode during field-ionization. The design emphasizes user-friendly operation by simplifying the sample exchange and by reducing the chamber volume under vacuum for a faster turn-around time between experiments. The proposed design is highly modular, allowing for easy installation of additional analytic capabilities and other future upgrades. | en_US |
dc.description.uri | http://archive.org/details/designndinstalla1094510574 | |
dc.format.extent | xvi, 75 p. : ill. (chiefly col.) ; 28 cm. | en_US |
dc.publisher | Monterey, California. Naval Postgraduate School | en_US |
dc.rights | This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States. | en_US |
dc.subject.lcsh | Astronautics. | en_US |
dc.title | Design and installation of a field ionization test chamber for ion thrusters | en_US |
dc.contributor.secondreader | Biblarz, Oscar | |
dc.contributor.department | Mechanical and Aerospace Engineering (MAE) | |
dc.subject.author | carbon nanotube | en_US |
dc.subject.author | ion thruster | en_US |
dc.subject.author | nanosatellite | en_US |
dc.subject.author | test chamber | en_US |
dc.description.service | US Navy (USN) author | en_US |
etd.thesisdegree.name | M.S. in Astronautical Engineering | en_US |
etd.thesisdegree.level | Masters | en_US |
etd.thesisdegree.discipline | Astronautical Engineering | en_US |
etd.thesisdegree.grantor | Naval Postgraduate School (U.S.) | en_US |
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