US4387467A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Satellite test chamber with electromagnetic reflection and resonance damping for simulating system generated electromagnetic pulses
Assignee: United States Department of the Air Force
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Filing: 1981-07-27
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Granted: 1983-06-07
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Expires: 2001-07-27
Abstract
Abstract The simulation of systems generated electromagnetic pulses in a space environment for satellite testing is accomplished by means of a spherical test chamber that is coupled with a pulsed x-ray source. Resonance damping is provided by a spherical resistive resonance suppression grid that is placed within the test chamber and spaced from its inner surface by a distance that effects optimum damping of electromagnetic wave energy at the fundamental chamber standing wave frequency. Electrons generated from surfaces within the chamber are suppressed by a spherical resistive electron backscatter suppression grid disposed between the resonance suppression grid and the chamber inner wall and by coating the inner chamber wall with electron emission suppression material.
Inventors
- 👤 William G. Kirby
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 05:32
CPC Classifications
G; G01; G01R; G01R29/00; G01R29/08; G01R29/10; G01R29/105
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
112 words
A satellite test chamber for simulating system generated electromagnetic pulses comprising a spherical chamber, means for holding a satellite to be tested at the center of said chamber, an X-ray source for generating high power X-ray pulses positioned to direct X-ray pulses generated thereby to the center of said chamber and onto a satellite disposed thereat, said X-ray source and said spherical chamber being integrated to form a hermetically sealed system, vacuum means for evacuating said hermetically sealed system, and a spherical resistive resonance suppression grid within and concentric with said spherical chamber, said resonance suppression grid being physically spaced from the inner surface of said spherical chamber and electrically isolated therefrom.
Claim 2
Dependent Claim
112 words
A satellite test chamber for simulating system generated electromagnetic pulses comprising a spherical chamber, means for holding a satellite to be tested at the center of said chamber, an X-ray source for generating high power X-ray pulses positioned to direct X-ray pulses generated thereby to the center of said chamber and onto a satellite disposed thereat, said X-ray source and said spherical chamber being integrated to form a hermetically sealed system, vacuum means for evacuating said hermetically sealed system, and a spherical resistive resonance suppression grid within and concentric with said spherical chamber, said resonance suppression grid being physically spaced from the inner surface of said spherical chamber and electrically isolated therefrom.
Claim 3
Dependent Claim
34 words
A satellite test chamber as defined in claim 1 wherein said spherical resistive resonance suppression grid has a radius that effects optimum damping of electromagnetic wave energy at the fundamental chamber standing wave frequency.
Claim 4
Dependent Claim
25 words
a satellite test chamber as defined in claim 2 including a coating of electron emission suppression material on the inner surface of said spherical chamber.
Claim 5
Dependent Claim
29 words
A satellite test chamber as defined in claim 3 including a spherical resistive electron backscatter suppression grid disposed between said spherical resistive resonance suppression grid and said spherical chamber.
Claim 6
Dependent Claim
42 words
A satellite test chamber as defined in claim 4 wherein the grid wires of said resonance suppression grid and said electron backscatter suppression grid are spaced at approximately 0.75 inches and the impedance of each grid is substantially 200 ohms per square.
Claim 7
Dependent Claim
36 words
A satellite test chamber as defined in claim 5 wherein said electron backscatter suppression grid and said resonance suppression grid are spaced approximately 0.13 and 0.20 radii respectively from the inner surface of said spherical chamber.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1986-06-06 | 1986-12-06 | 1987-06-07 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-06-06 | 1990-12-06 | 1991-06-07 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-06-06 | 1994-12-06 | 1995-06-07 | $7700.00 | Window Closed / Lapsed |