Abstract: A specially designed magnetic shunt is provided encircling the anode region and/or annular gas distribution area of an ion accelerator with closed electron drift. The magnetic shunt is constructed to concentrate the magnetic field at the ion exit end, such that the location of maximum magnetic field strength is located downstream from the inner and outer magnetic poles of the accelerator. The specially designed shunt also results in desired curvatures of magnetic field lines upstream of the line of maximum magnetic field strength, to achieve a focusing effect for increasing the life and efficiency of accelerator.
Type:
Grant
Filed:
November 13, 1998
Date of Patent:
March 27, 2001
Assignee:
Primex Aerospace Company
Inventors:
David Q. King, Kristi H. de Grys, Randall S. Aadland, Dennis L. Tilley, Arnold W. Voigt