Title :
Ion acceleration in a radio frequency driven ferroelectric plasma source
Author_Institution :
Electr. & Comput. Eng. Dept., Univ. of Missouri, Columbia, MO, USA
fDate :
4/1/2005 12:00:00 AM
Abstract :
Ion emission from ferroelectric plasma sources driven by radio frequency (RF) applied voltage is studied. An experimental investigation of particle emission from lead zirconate titanate ferroelectric ceramics driven by bursts of seven cycles of RF voltage at 248 kHz has revealed significant ion current emission. Measured electron to ion peak current ratios ranged from 11 to 19, which is much lower than the expected thermal current ratio. These results indicate that the ions are being preferentially accelerated. An analysis of the ponderomotive force on the ions and electrons reveals that it may be responsible for acceleration of the ions. The ferroelectric plasma is examined as a possible micropropulsion thruster. Performance estimates based on the ponderomotive acceleration calculations predict specific impulse of 2000-3000 s, thrust of 0.1-1 mN, and specific power of 15 W/mN. These estimates are compared to existing micropropulsion concepts, revealing the attractiveness of ferroelectric plasma sources.
Keywords :
aerospace propulsion; ferroelectric ceramics; ferroelectric devices; lead compounds; plasma accelerators; plasma dielectric properties; plasma nonlinear processes; plasma sources; 2000 to 3000 s; 248 kHz; PZT; PbZrO3TiO3; electron-to-ion peak current ratios; ion acceleration; ion current emission; lead zirconate titanate ferroelectric ceramics; micropropulsion thruster; particle emission; ponderomotive force; radiofrequency driven ferroelectric plasma source; thermal current ratio; Acceleration; Ceramics; Current measurement; Electrons; Ferroelectric materials; Ion emission; Plasma sources; Radio frequency; Titanium compounds; Voltage; Ferroelectric devices; ion sources; plasma engines; space vehicle propulsion;
Journal_Title :
Plasma Science, IEEE Transactions on
DOI :
10.1109/TPS.2005.844592