Ion thruster with ion-extraction grids having compound contour shapes

• US 6,250,070 B1
• Filed: 05/09/2000
• Issued: 06/26/2001
• Est. Priority Date: 05/09/2000
• Status: Expired due to Fees

• Current Assignee: L-3 Communications Electron Technologies, Inc. (L3Harris Technologies, Inc.)
• Original Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Inventors: Wittmann, Alois, Kreiner, Kurt B., Pilcher, Lewis S., Beattie, John R.
• Primary Examiner(s): KIM, TAE JUN
• Application Number:
  US09/569,708
• Time in Patent Office: 413 Days
• Field of Search: 602/02, 313/360.1, 313/359.1, 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
• CPC Class Codes: H01J 27/024 Extraction optics, e.g. grids
• CPC Class Codes: H05H 1/54 Plasma accelerators

Abstract

An ion thruster has a source of a plasma, and an ion-optics system located in sufficient proximity to the source of the plasma to extract ions therefrom. The ion-optics system includes at least two grids arranged in a facing-but-spaced-apart relationship to each other, with each grid being axisymmetric about a grid axis. Each grid includes a peripheral region defining a grid plane perpendicular to the grid axis, a first region of curvature adjacent to the peripheral region, and a second region of curvature along the grid axis such that the first region of curvature lies between the second region of curvature and the peripheral region. The first region of curvature is a convexly curved segment of a first sphere relative to the grid plane, and the second region of curvature is a concavely curved segment of a second sphere relative to the grid plane.

Claims

1. An ion thruster, comprising:

a source of a plasma; and

an ion-optics system located in sufficient proximity to the source of the plasma to extract ions therefrom along a thrust axis, the ion-optics system comprising at least two grids arranged in a facing-but-spaced-apart relationship to each other, each grid comprising

a peripheral region defining a grid plane perpendicular to the thrust axis,

a first region of curvature adjacent to the peripheral region, the first region of curvature being convexly curved relative to the grid plane, and

a second region of curvature along the thrust axis such that the first region of curvature lies between the second region of curvature and the peripheral region, the second region of curvature being concavely curved relative to the grid plane.

2. The ion thruster of claim 1, wherein the first region of curvature is a segment of a first sphere.

3. The ion thruster of claim 1, wherein the second region of curvature is a segment of a second sphere.

4. The ion thruster of claim 1, wherein the first region of curvature is a segment of a first sphere and the second region of curvature is a segment of a second sphere.

5. The ion thruster of claim 1, wherein the first sphere and the second sphere have substantially the same radius of curvature R, wherein each grid has a diameter D_G measured in the grid plane, and wherein R/D_G is about 2/1.

6. The ion thruster of claim 1, wherein each grid further comprises a third region of curvature lying between the first region of curvature and the second region of curvature.

7. The ion thruster of claim 1, wherein the first region of curvature is bowed outwardly relative to the grid plane.

8. The ion thruster of claim 1, wherein the first region of curvature is bowed inwardly relative to the grid plane.

9. The ion thruster of claim 1, wherein there are exactly two grids.

10. The ion thruster of claim 1, wherein there are exactly three grids.

11. The ion thruster of claim 1, wherein each grid further comprises:

at least two mounting ears affixed to the peripheral region of the grid at a location remote from the first region of curvature.

12. An ion thruster, comprising:

a source of a plasma; and

an ion-optics system located in sufficient proximity to the source of the plasma to extract ions therefrom, the ion-optics system comprising at least two grids arranged in a facing-but-spaced-apart relationship to each other, each grid being axisymmetric about a grid axis and comprising

a peripheral region defining a grid plane perpendicular to the grid axis,

a first region of curvature adjacent to the peripheral region, the first region of curvature being a convexly curved segment of a first sphere relative to the grid plane, and

a second region of curvature along the grid axis such that the first region of curvature lies between the second region of curvature and the peripheral region, the second region of curvature being a concavely curved segment of a second sphere relative to the grid plane.

13. The ion thruster of claim 12, wherein

each grid has a diameter measured in the grid plane of D_G,

the first-sphere radius of curvature is R, and

the ratio R/D_G is about 2/1.

14. The ion thruster of claim 12, wherein each grid further comprises

a third region of curvature lying between the first region of curvature and the second region of curvature.

15. The ion thruster of claim 12, wherein there are exactly two grids.

16. The ion thruster of claim 12, wherein there are exactly three grids.

17. The ion thruster of claim 12, wherein the first region of curvature is bowed outwardly relative to the grid plane.

18. The ion thruster of claim 12, wherein the first region of curvature is bowed inwardly relative to the grid plane.