Magnetically Conformed, Variable-Area Discharge Chamber for Hall Thruster, and Method

TBMG-26856

05/01/2017

Abstract
Content

NASA's Jet Propulsion Laboratory has developed a Hall thruster with a variable-area discharge chamber that improves the performance and lifetime of the thruster. Conventional Hall thrusters have poor ionization efficiency, which limits the thrust-to-power ratio that can be achieved with the thruster. JPL's novel Hall thruster has a variable-area discharge chamber that conforms to the curvature of the local magnetic field and optimizes the ionization efficiency of the thruster and, therefore, significantly improves the power-to-thrust ratio that can be achieved. This innovative device decreases spacecraft costs and enables fast, efficient orbit transfers.

Meta TagsDetails
Citation
"Magnetically Conformed, Variable-Area Discharge Chamber for Hall Thruster, and Method," Mobility Engineering, May 1, 2017.
Additional Details
Publisher
Published
May 1, 2017
Product Code
TBMG-26856
Content Type
Magazine Article
Language
English