Ion thruster with long-lifetime ion-optics system

• US 5,924,277 A
• Filed: 12/17/1996
• Issued: 07/20/1999
• Est. Priority Date: 12/17/1996
• Status: Expired due to Term

• Current Assignee: L-3 Communications Electron Technologies, Inc. (L3Harris Technologies, Inc.)
• Original Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Inventors: Williams, John D., Beattie, John R., Matossian, Jesse N.
• Primary Examiner(s): Thorpe, Timothy S.
• Assistant Examiner(s): KIM, TAE JUN
• Application Number:
  US08/767,920
• Time in Patent Office: 945 Days
• Field of Search: 60/202, 313/359.1, 313/360.1, 313/361.1, 313/362.1, 315/111.81
• US Class Current: 60/202
• CPC Class Codes: F03H 1/0043 characterised by the acceleration grid extraction optics for ion sources H01J27/024

Abstract

Ion erosion of grids is reduced in an ion thruster with a multiple-grid ion-optics system. The thruster has an array of aperture sets in which aperture areas change in a perimeter region of the array. In one ion-optics system embodiment, a screen aperture area is reduced and a decelerator aperture area is increased in aperture sets that are proximate to the perimeter of the array. Prototype tests of this embodiment have illustrated significant reduction of ion erosion.

Claims

1. A multiple-grid ion-optics system for generating ion beamlets from a plasma source in an ion thruster, comprising:

a screen grid;

an accelerator grid spaced from said screen grid;

a decelerator grid spaced from said accelerator grid and positioned so that said accelerator grid is between said screen grid and said decelerator grid; and

an array of aperture sets, said array having an array perimeter and said aperture sets divided into a first group of aperture sets and a second group of aperture sets that are proximate to said array perimeter and that surround said first group and each of said aperture sets including;

a screen aperture formed by said screen grid to facilitate the flow of a respective one of said ion beamlets from said plasma source, wherein said screen aperture has a first screen aperture area in said first group and a second screen aperture area in said second group which is reduced from said first screen aperture area;

an accelerator aperture formed by said accelerator grid to have an accelerator aperture area and positioned so that an accelerator voltage on said accelerator grid attracts said respective ion beamlet and accelerates it through said accelerator aperture, wherein said accelerator aperture area is constant throughout said first and second groups; and

a decelerator aperture formed by said decelerator grid to have a decelerator aperture area and positioned so that a decelerator voltage on said decelerator grid at least partially collimates said respective ion beamlet, wherein said decelerator aperture area is constant throughout said first and second groups;

the reduced second screen aperture area reducing ion erosion of said decelerator grid.

2. The multiple-grid ion-optics system of claim 1, wherein said second group of aperture sets includes N subgroups whose second screen aperture areas monotonically decrease with increasing proximity to said perimeter.

3. The multiple-grid ion-optics system of claim 1, wherein said screen aperture, said accelerator aperture and said decelerator aperture each have a circular cross section.

4. The multiple-grid ion-optics system of claim 1, wherein said screen aperture, said accelerator aperture and said decelerator aperture each have a hexagonal cross section.

5. The multiple-grid ion-optics system of claim 1, wherein the aperture sets of said array are arranged in rows with a first plurality of said rows offset from a second plurality of said rows.

6. The multiple-grid ion-optics system of claim 1, wherein said screen grid, said accelerator grid and said decelerator grid have a spherical configuration to enhance their thermal stability.

7. The multiple-grid ion-optics system of claim 1, wherein said array has a circular configuration.

8. A multiple-grid ion-optics system for generating ion beamlets from a plasma source in an ion thruster, comprising:

a screen grid;

an accelerator grid spaced from said screen grid;

a decelerator grid spaced from said accelerator grid and positioned so that said accelerator grid is between said screen grid and said decelerator grid; and

an array of aperture sets, said array having an array perimeter and said aperture sets divided into a first group of aperture sets and a second group of aperture sets that are proximate to said array perimeter and that surround said first group and each of said aperture sets including;

a screen aperture formed by said screen grid to facilitate the flow of a respective one of said ion beamlets from said plasma source and having a screen aperture area that is constant throughout said first and second groups;

an accelerator aperture formed by said accelerator grid to have an accelerator aperture area and positioned so that an accelerator voltage on said accelerator grid attracts said respective ion beamlet and accelerates it through said accelerator aperture, wherein said accelerator aperture area is constant throughout said first and second groups; and

a decelerator aperture formed by said accelerator grid and positioned so that a decelerator voltage on said decelerator grid at least partially collimates said respective ion beamlet, said decelerator aperture having a first decelerator aperture area in said first group and a second decelerator aperture area in said second group which is increased from said first decelerator aperture area;

the increased second decelerator aperture area reducing ion erosion of said decelerator grid.

9. The multiple-grid ion-optics system of claim 8, wherein said second group of aperture sets includes N subgroups whose second decelerator aperture areas monotonically increase with increasing proximity to said perimeter.

10. The multiple-grid ion-optics system of claim 8, wherein said screen aperture, said accelerator aperture and said decelerator aperture each have a circular cross section.

11. The multiple-grid ion-optics system of claim 8, wherein said screen aperture, said accelerator aperture and said decelerator aperture each have a hexagonal cross section.

12. An ion thruster for generating an ion beam which is formed from a plurality of ion beamlets, comprising:

a housing;

a chamber formed by said housing for receiving an ionizable gas, said chamber having an open end;

an electron source positioned to inject primary electrons into said chamber;

an electrode system positioned in said chamber to receive electrode voltages for acceleration of said primary electrons and ionization of said gas into a plasma source;

a magnet system positioned in said chamber and configured to generate magnetic field lines proximate to said housing to enhance said ionization;

a multiple-grid ion-optics system positioned across said open end and having;

a screen grid;

an accelerator grid spaced from said screen grid;

a decelerator grid spaced from said accelerator grid and positioned so that said accelerator grid is between said screen grid and said decelerator grid; and

an array of aperture sets, said array having an array perimeter and said aperture sets divided into a first group of aperture sets and a second group of aperture sets that are proximate to said array perimeter and that surround said first group and each of said aperture sets including;

a screen aperture formed by said screen grid to facilitate the flow of a respective one of said ion beamlets from said plasma source, wherein said screen aperture has a first screen aperture area in said first group and a second screen aperture area in said second group which is reduced from said first screen aperture area;

an accelerator aperture formed by said accelerator grid to have an accelerator aperture area and positioned so that an accelerator voltage on said accelerator grid attracts said respective ion beamlet and accelerates it through said accelerator aperture, wherein said accelerator aperture area is constant throughout said first and second groups; and

a decelerator aperture formed by said decelerator grid to have a decelerator aperture area and positioned so that a decelerator voltage on said decelerator grid at least partially collimates said respective ion beamlet, wherein said decelerator aperture area is constant throughout said first and second groups;

and

a neutralizer configured and positioned to inject neutralizing electrons into a region which is proximate to said ion beamlets.

13. The ion thruster of claim 12, wherein said electrode system includes:

a hollow cathode positioned in said chamber; and

an anode positioned proximate to said housing.

14. The ion thruster of claim 12, wherein said magnet system includes a plurality of annular permanent magnets positioned proximate to said housing.

15. The ion thruster of claim 12, further including a power supply system configured to supply said accelerator voltage and said decelerator voltage.

16. The ion thruster of claim 12, further including:

a vessel for containing a supply of said ionizable gas; and

a flow orifice coupled between said chamber and said vessel for delivering ionizable gas to said chamber.

17. The ion thruster of claim 12, wherein said neutralizer includes:

a source of neutralizing electrons; and

an neutralizer electrode positioned to receive a neutralizer voltage for injection of said neutralizing electrons.

18. An ion thruster for generating an ion beam which is formed from a plurality of ion beamlets, comprising:

a housing;

a chamber formed by said housing for receiving an ionizable gas, said chamber having an open end;

an electron source positioned to inject primary electrons into said chamber;

an electrode system positioned in said chamber to receive electrode voltages for acceleration of said primary electrons and ionization of said gas into a plasma source;

a magnet system positioned in said chamber and configured to generate magnetic field lines proximate to said housing to enhance said ionization;

a multiple-grid ion-optics system positioned across said open end and having;

a screen grid;

an accelerator grid spaced from said screen grid;

a decelerator grid spaced from said accelerator grid and positioned so that said accelerator grid is between said screen grid and said decelerator grid; and

an array of aperture sets, said array having an array perimeter and said aperture sets divided into a first group of aperture sets and a second group of aperture sets that are proximate to said array perimeter and that surround said first group and each of said aperture sets including;

a screen aperture formed by said screen grid to facilitate the flow of a respective one of said ion beamlets from said plasma source and having a screen aperture area that is constant throughout said first and second groups;

an accelerator aperture formed by said accelerator grid to have an accelerator aperture area and positioned so that an accelerator voltage on said accelerator grid attracts said respective ion beamlet and accelerates it through said accelerator aperture, wherein said accelerator aperture area is constant throughout said first and second groups; and

a decelerator aperture formed by said accelerator grid and positioned so that a decelerator voltage on said decelerator grid at least partially collimates said respective ion beamlet, said decelerator aperture having a first decelerator aperture area in said first group and a second decelerator aperture area in said second group which is increased from said first decelerator aperture area;

and

a neutralizer configured and positioned to inject neutralizing electrons into a region which is proximate to said ion beamlets.

19. The ion thruster of claim 18, wherein said electrode system includes:

a hollow cathode positioned in said chamber; and

an anode positioned proximate to said housing.

20. The ion thruster of claim 18, wherein said magnet system includes a plurality of annular permanent magnets positioned proximate to said housing.