Hall thruster with annular cathode

Patent metadata

Field	Value
Publication number	US-11486371-B2
Application number	US-201716771026-A
Country	US
Kind code	B2
Filing date	Dec 19, 2017
Priority date	Dec 19, 2017
Publication date	Nov 1, 2022
Grant date	Nov 1, 2022

Abstract

A Hall thruster includes an annular discharge region and an annular cathode concentric to the annular discharge region.

First claim

What is claimed is:

1. A Hall thruster comprising:
a magnetic pole disposed about a central axis;
a passage along the central axis through the magnetic pole;
an annular discharge region;
an anode, wherein at least a portion of the anode is disposed in the annular discharge region; and
an annular cathode in the form of a ring concentric to the annular discharge region around the central axis, wherein the annular cathode is radially inwardly displaced from the annular discharge region and radially outwardly displaced from the passage.

2. The Hall thruster as recited in claim 1 , wherein the annular cathode is circumscribed by the annular discharge region.

3. The Hall thruster as recited in claim 1 , further comprising another portion of the anode surrounding the annular discharge region.

4. The Hall thruster as recited in claim 1 , wherein the annular cathode is circumscribed by the annular discharge region.

5. The Hall thruster as recited in claim 1 , wherein a radially outer surface of the ring is substantially equidistant from the discharge region.

6. The Hall thruster as recited in claim 1 , wherein the anode and the annular cathode are electrically coupled to generate an electric field there between and induce electrons to drift into the annular discharge region.

7. A Hall thruster comprising:
a radially inner magnetic pole and a radially outer magnetic pole, wherein the radially inner magnetic pole and the radially outer magnetic pole are disposed about a central axis;
a passage along the central axis through the radially inner magnetic pole;
an annular discharge region between the radially inner magnetic pole and the radially outer magnetic pole;
a propellant gas feeder operable to feed propellant gas to the annular discharge region;
an annular cathode in the form of a ring concentric to the annular discharge region around the central axis, wherein the annular cathode is radially inwardly displaced from the annular discharge region and radially outwardly displaced from the passage;
an anode disposed in the annular discharge region; and
at least one magnet magnetically coupled with the radially inner magnetic pole and the radially outer magnetic pole to generate a magnetic field across the annular discharge region.

8. The Hall thruster as recited in claim 7 , wherein the annular cathode is circumscribed by the annular discharge region.

Assignees

• Aerojet Rocketdyne Inc

Inventors

• Pucci Justin

Classifications

• F03H1/0037 Primary

  Electrostatic ion thrusters · CPC title

• F03H1/0025

  Neutralisers, i.e. means for keeping electrical neutrality · CPC title

• F03H1/0075 Primary

  with an annular channel; Hall-effect thrusters with closed electron drift · CPC title