Method for making an ion thruster grid

• US 5,551,904 A
• Filed: 06/05/1995
• Issued: 09/03/1996
• Est. Priority Date: 02/26/1993
• Status: Expired due to Fees

• Current Assignee: Government of the United States of America
• Original Assignee: The Boeing Co.
• Inventors: Rorabaugh, Michael E., Hedges, Daniel E., Meserole, Jere S. Jr.
• Primary Examiner(s): Ramsey, Kenneth J.
• Application Number:
  US08/463,581
• Time in Patent Office: 456 Days
• Field of Search: 445/46, 445/47, 264/29.2, 264/29.5
• US Class Current: 445/47
• 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

Abstract

Carbon-carbon grids for ion optics sets are thermomechanically stable under the extreme temperature changes that are experienced in ion thrusters. Screen, accelerator and decelerator grids are thermomechanically stable, lightweight, and resistant to erosion from ion sputtering and have extended lifetimes over conventional molybdenum grids.

Claims

1. A process for manufacturing a carbon-carbon grid element of an ion optics set for an ion beam source comprising the steps of:

positioning at least two layers of carbon fibers in a crossing or woven array;

embedding the array of carbon fibers in a carbon matrix; and

creating apertures in the carbon matrix between the carbon fibers.

2. The process of claim 1, further comprising the step of infiltrating with carbon any voids left in the grid element after the apertures are created.

3. The process of claim 1, wherein the step of providing apertures further comprises providing rectangular apertures in orthogonal rows and columns.

4. The process of claim 1, wherein the step of providing apertures further comprises the steps of:

positioning inserts corresponding to the apertures on a formboard;

positioning the carbon fibers around the inserts; and

removing the inserts and formboard following the embedding step.

5. The process of claim 1, wherein positioning the fibers further comprises arranging a plurality of the sheets in at least two different directions relative to the direction of the weave.

6. The process of claim 1, wherein the infiltrating step is accomplished using a technique selected from the group consisting of pitch infiltration, resin infiltration, chemical vapor infiltration, or a combination thereof.

7. A carbon-carbon grid element manufactured in accordance with the process of claim 6.