Development and Testing of a Field Ionized Ion Thruster for Microsatellite Applications

Development of a miniaturized ion thruster would enable microsatellites to sustain orbits over a long period of time with a high efficiency while minimizing mass and volume. The advent of carbon nanotube technology has made the development of a field ionized ion thruster possible. An interagency eff...

Full description

Bibliographic Details
Main Author: Shrank, Bryan P.
Other Authors: Romano, Marcello
Published: Monterey, California. Naval Postgraduate School 2014
Online Access:http://hdl.handle.net/10945/43382