Hall effect thruster with anode having magnetic field barrier
View Patent ↗An efficiency enhancing anode-magnetic structure of a Hall effect thruster produces a radially directed magnetic field between inner and outer poles at the exit portion of a gas distribution channel. The field-shaping structure includes magnetic material extending alongside the channel with an associated secondary flux-generating component to create an axially directed magnetic field in the area between the anode of the thruster and the exit portion of the gas distribution channel.
1. A Hall effect ion accelerator having an annular gas discharge channel including an exit end portion, discharge of gas through the exit end portion defining a downstream direction, said accelerator comprising:
an inner magnetic pole located at the inside of and encircled by the annular gas discharge area adjacent to the exit end portion;
an outer magnetic pole located at the outside of and encircling the annular gas discharge area adjacent to the exit end portion, the inner and outer magnetic poles being magnetically coupled by a first magnetic path;
a first magnetic field source associated with the first magnetic path for producing a generally radially extending magnetic field between the inner pole and the outer pole at the exit end portion of the gas discharge channel;
an anode located upstream of the exit end portion of the gas discharge channel;
a gas source for supplying an ionizable gas to the gas discharge channel for flow in a downstream direction toward the exit end portion;
an electron source for supplying free electrons for introduction through the exit end portion of the gas discharge channel in a generally upstream direction;
an electric field source for producing an electric field extending from the anode in a downstream direction toward the exit end portion of the gas discharge channel, interaction between the ionizable gas from the gas source and free electrons from the electron source providing ions accelerated in a downstream direction by the electric field;
an outer shell of magnetic material having a downstream end adjacent to the innermost part of the outer pole and extending upstream therefrom along an outer portion of the gas discharge channel;
an inner shell of magnetic material having a downstream end adjacent to the outermost part of the inner pole and extending upstream therefrom along an inner portion of the gas discharge channel, the outer and inner shells being magnetically coupled behind the anode to define a second magnetic path and the magnetic material of the second path being concentrated in an area upstream of the anode; and
a second magnetic field source associated with the second magnetic path and generating magnetic flux therealong sufficient to generate magnetic field lines extending generally axially in the gas discharge channel from a location adjacent to the anode and downstream toward the exit end portion of the gas discharge channel to enhance election mobility in an area between the anode and the exit end portion of the gas discharge channel.
2. The accelerator defined in claim 1 , in which the magnetic field in the gas discharge channel induced by the first magnetic field source and second magnetic field source transitions abruptly from a generally radial direction at the exit end portion to a generally axial direction upstream from the exit end portion.