Hall effect thruster and a space vehicle including such a thruster

Patent metadata

Field	Value
Publication number	US-10131453-B2
Application number	US-201615547360-A
Country	US
Kind code	B2
Filing date	Jan 28, 2016
Priority date	Jan 30, 2015
Publication date	Nov 20, 2018
Grant date	Nov 20, 2018

Abstract

A Hall effect thruster arranged inside a wall and including a magnetic circuit and an electric circuit including an anode, a first cathode, and a voltage source. The magnetic circuit and the electric circuit are arranged in such a manner as to generate magnetic and electric fields around the wall. In every meridian section, the magnetic circuit presents an upstream magnetic pole and a downstream magnetic pole arranged at the surface of the wall and spaced apart from each other; and the anode and the first cathode are situated on either side of the upstream magnetic pole.

First claim

The invention claimed is:

1. A Hall effect thruster for accelerating ions to develop thrust along a thrust axis comprising:
a magnetic circuit for generating a magnetic field; and
an electric circuit comprising an anode, a first cathode, and a voltage source for emitting electrons via at least the first cathode and attracting electrons via the anode;
wherein:
the magnetic circuit is arranged radially inside a wall formed around the thrust axis and the anode and the first cathode lie along the wall;
the magnetic circuit and the electric circuit are arranged so as to generate magnetic and electric fields surrounding and radially outward of the wall; and
the magnetic circuit presents an upstream magnetic pole and a downstream magnetic pole arranged at a surface of the wall and spaced apart; and
the anode and the first cathode are situated on either side of the upstream magnetic pole, wherein acceleration of the ions occurs outside of the Hall effect thruster entirely radially outward of the wall.

2. The Hall effect thruster according to claim 1 , wherein the magnetic circuit is arranged in such a manner that the magnetic field is oriented in a direction that is perpendicular to the surface of the wall, next to the upstream magnetic pole.

3. The Hall effect thruster according to claim 1 , wherein the electric circuit also includes a second cathode arranged axially between the upstream magnetic pole and the downstream magnetic pole.

4. The Hall effect thruster according to claim 1 , wherein the electric circuit also includes an additional cathode arranged axially downstream from the downstream magnetic pole.

5. The Hall effect thruster according to claim 1 , wherein the voltage source is controllable, it being possible to reverse the voltage of the voltage source in order to reverse the thrust of the Hall effect thruster.

6. The Hall effect thruster according to claim 1 , wherein the magnetic circuit and/or the electric circuit is/are arranged in such a manner as to generate a non-axisymmetric magnetic and/or electric field around the wall.

7. A space vehicle including at least one Hall effect thruster according to claim 1 .

Assignees

• Safran Aircraft Engines

Inventors

• Marchandise Frederic Raphael Jean
• Vial Vanessa
• Zurbach Stephan

Classifications

• F03H1/0062 Primary

  grid-less with an applied magnetic field · CPC title

• H05H1/54 Primary

  Plasma accelerators · CPC title

• F03H1/0012

  Means for supplying the propellant · CPC title

• F03H1/0006 Primary

  Details applicable to different types of plasma thrusters (arrangements specially adapted for fitting plasma engines in or to cosmonautic vehicles B64G1/413) · CPC title

• F03H1/0068

  with a central channel, e.g. end-Hall type · CPC title