DocumentCode :
3507789
Title :
Characterization of simulated ion beam neutralization stability in two and three dimensions
Author :
Wheelock, A. ; Cooke, D.L. ; Gatsonis, N.A.
Author_Institution :
Space Vehicles Directorate, Air Force Res. Lab., Hanscom AFB, MA, USA
fYear :
2004
fDate :
1-1 July 2004
Firstpage :
324
Abstract :
Summary form only given. The ready neutralization of ion beams given a source of electrons is well known, but the physics of that process are not clearly understood. Ion and electron currents must be matched to prevent spacecraft charging while space charge neutrality is required in the beam to prevent reflection. These are often thought of as two separate processes, yet the reality that the system is quite robust indicates that there is a physical mechanism to couple them. With electric propulsion moving into both the micro and macro ranges with colloids, FEEPs and thruster arrays, predicting the behavior of neutralizing electrons and plume ions is of increasing importance. Simulations using 2D and 3D Particle-in-Cell (PIC) codes are presented, detailing starting and steady state conditions of an ion beam. It is shown that at steady state, simulations are ultimately nearly space charge neutral regardless of ion or electron currents, while simulations using starting conditions require detailed current balance to propagate without space charge barriers. Further investigation of the steady state reveals that standard PIC provides no mechanism for imparting bulk ion velocity to electrons to provide both space charge and current coupling without a careful balance of the source conditions, such as the electron temperature, contrary to observations.
Keywords :
electric propulsion; ion engines; plasma instability; plasma simulation; plasma temperature; plasma transport processes; space charge; space vehicles; bulk ion velocity; electric propulsion; electron current; electron temperature; ion current; neutralizing electrons; particle-in-cell code; plume ions; simulated ion beam neutralization stability; space charge neutrality; spacecraft charging; three dimensional PIC code; two dimensional PIC code; Electron beams; Ion beams; Optical reflection; Physics; Propulsion; Robustness; Space charge; Space vehicles; Stability; Steady-state;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Plasma Science, 2004. ICOPS 2004. IEEE Conference Record - Abstracts. The 31st IEEE International Conference on
Conference_Location :
Baltimore, MD, USA
ISSN :
0730-9244
Print_ISBN :
0-7803-8334-6
Type :
conf
DOI :
10.1109/PLASMA.2004.1340021
Filename :
1340021
Link To Document :
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