Low-power hall thruster

摘要

A low power hall thruster is provided that is effective for micro-spacecrafts and nano-spacecrafts as well as mini-spacecrafts. The hall thruster comprises a co-axial acceleration channel capable of being applied with predominantly-radial magnetic field and a co-axial anode within a cavity capable of being applied with substantially longitudinal magnetic field. A cathode-compensator is placed beyond the acceleration channel and magnetic system is provided capable of generating the radial magnetic field within the co-axial acceleration channel and the longitudinal magnetic field within the co-axial anode. An electrically isolated gas distributor is also provided.

主权项

1. A Hall thruster comprising:
an acceleration channel extending along an axial direction having a first end arid a second end opposite to each other; an elongated anode extending along the axial direction positioned at said first end of said acceleration channel, said anode comprising working surfaces of two coaxial cylinders defining a cavity between said working surfaces and an exit for ions moving towards said acceleration channel predominantly along the axial direction with respect to said cylinders, wherein an electric field formed in said cavity has a radial component directed to prevent the ions in said cavity from attaining said working surfaces of said cylinders; a cathode-compensator, placed at said second end of said acceleration channel; a magnetic system generating a predominately radial magnetic field within said acceleration channel and a predominantly longitudinal magnetic field within said cavity of said anode; and a gas distributor, placed in said cavity of said anode between said working surfaces, opposite to said exit, and being electrically isolated from said anode, said cathode-compensator and said magnetic system.