Claims
- 1. A passive intermodulation shield comprising:
- a substrate; and
- a conducting layer deposited over the substrate to produce a surface resistivity between 2 ohms per square and 200 ohms per square;
- wherein the surface resistivity is greater than 2 ohms per square to limit an amount of inherent passive intermodulation generation, and wherein the surface resistivity is less than 200 ohms per square to limit an amount of passive intermodulation passthrough.
- 2. The passive intermodulation shield of claim 1 wherein the substrate includes a polyimide sheet.
- 3. The passive intermodulation shield of claim 1 wherein the substrate includes a Kapton sheet.
- 4. The passive intermodulation shield of claim 1 wherein the surface resistivity is between 4 ohms per square and 100 ohms per square.
- 5. The passive intermodulation shield of claim 1 wherein the surface resistivity is between 10 ohms per square and 40 ohms per square.
- 6. The passive intermodulation shield of claim 1 wherein the surface resistivity is selected to maintain both the inherent passive intermodulation generation and the passive intermodulation passthrough below a predetermined value.
- 7. The passive intermodulation shield of claim 6 wherein the surface resistivity is selected to maintain both the inherent passive intermodulation generation and the passive intermodulation passthrough below -20 dB.
- 8. The passive intermodulation shield of claim 6 wherein the surface resistivity is selected to maintain both the inherent passive intermodulation generation and the passive intermodulation passthrough below -35 dB.
- 9. The passive intermodulation shield of claim 6 wherein the surface resistivity is selected to maintain both the inherent passive intermodulation generation and the passive intermodulation passthrough below -55 dB.
- 10. The passive intermodulation shield of claim 1 wherein the surface resistivity is selected to be near-optimal in minimizing the maximum of the inherent passive intermodulation generation and the passive intermodulation passthrough.
- 11. The passive intermodulation shield of claim 1 wherein the surface resistivity is selected so that the inherent passive intermodulation generation is approximately equal to the passive intermodulation passthrough.
- 12. A passive intermodulation shield for a spacecraft, the passive intermodulation shield comprising:
- a Kapton substrate; and
- a vacuum deposited aluminum layer over the substrate, the vacuum deposited aluminum layer having a thickness to produce a surface resistivity between 10 ohms per square and 40 ohms per square to maintain both an inherent passive intermodulation generation and a passive intermodulation passthrough to be below -55 dB.
- 13. A blanket for protecting a spacecraft from a space environment comprising:
- a pair of outer layers; and
- a passive intermodulation shield disposed between the pair of outer layers, the passive intermodulation shield having a conducting layer deposited over a substrate to produce a surface resistivity between 2 ohms per square and 200 ohms per square;
- wherein the surface resistivity is greater than 2 ohms per square to limit an amount of inherent passive intermodulation generation, and wherein the surface resistivity is less than 200 ohms per square to limit an amount of passive intermodulation passthrough.
- 14. The blanket of claim 13 wherein each of the pair of outer layers includes a respective plastic conductive sheet.
- 15. The blanket of claim 13 further comprising one or more vacuum deposited aluminum layers disposed between the passive intermodulation shield and a first of the pair of outer layers, wherein the passive intermodulation shield is operative to shield passive intermodulation generated by the one or more vacuum deposited aluminum layers.
- 16. The blanket of claim 13 wherein the surface resistivity is between 10 ohms per square and 40 ohms per square.
- 17. The blanket of claim 13 wherein the surface resistivity is selected to maintain both the inherent passive intermodulation generation and the passive intermodulation passthrough below a predetermined value.
- 18. The blanket of claim 13 wherein the surface resistivity is selected to maintain both the inherent passive intermodulation generation and the passive intermodulation passthrough below -55 dB.
- 19. The blanket of claim 13 wherein the surface resistivity is selected to be near-optimal in minimizing the maximum of the inherent passive intermodulation generation and the passive intermodulation passthrough.
- 20. The blanket of claim 13 wherein the surface resistivity is selected so that the inherent passive intermodulation generation is approximately equal to the passive intermodulation passthrough.
CROSS-REFERENCE TO RELATED APPLICATION
The present application is a continuation-in-part of copending U.S. application "Spacecraft Protective Blanket", having Ser. No. 07/784,338 filed on Oct. 29, 1991, and having the same assignee as the present application. The subject matter of the above-identified application is hereby incorporated by reference into the disclosure of the present application.
US Referenced Citations (6)
Foreign Referenced Citations (2)
Number |
Date |
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0356714 |
Jul 1989 |
EPX |
2469388 |
Nov 1980 |
FRX |
Non-Patent Literature Citations (3)
Entry |
Reeve, Ronald T.; Jet Propulsion Laboratory, California Institute of Technology, "Thermal Redesign of the Galileo Spacecraft for a VEEGA Trajectory," Journal of Spacecraft and Rockets (Mar./Apr., 1991). |
Stultz, James W.; Jet Propulsion Laboratory, California Institute of Technology; "Thermal Design of the Galileo Spun and Despun Science," Journal of Spacecraft and Rockets (Mar./Apr. 1991). |
Tsunoda, H., et al.; NTT Radio Communication Systems Laboratories, "Thermal Design Verification of a Large Depolyable Antenna for a Communications Satellite," Journal of Spacecraft and Rockets (Mar./Apr. 1992). |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
784338 |
Oct 1991 |
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