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Magnetically-conformed, Variable Area Discharge Chamber for Hall Thruster, and MethodThe invention is a Hall thruster that incorporates a discharge chamber having a variable area channel including an ionization zone, a transition region, and an acceleration zone. The variable area channel is wider through the acceleration zone than through the ionization zone. An anode is located in a vicinity of the ionization zone and a cathode is located in a vicinity of the acceleration zone. The Hall thruster includes a magnetic circuit which is capable of forming a local magnetic field having a curvature within the transition region of the variable area channel whereby the transition region conforms to the curvature of the local magnetic field. The Hall thruster optimizes the ionization and acceleration efficiencies by the combined effects of the variable area channel and magnetic conformity.
Document ID
20140001864
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Hofer, Richard R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
March 14, 2014
Publication Date
April 2, 2013
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-11/926,279
Patent Number: US-Patent-8,407,979
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,407,979
Patent Application
US-Patent-Appl-SN-11/926,279
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