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US3896758A Expired / Lapsed US ⏱️ 0.0 years remaining

Meteroroid impact position locator air for manned space station

Assignee: National Aeronautics and Space Administration
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Filing: 1973-10-02
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Granted: 1975-07-29
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Expires: 1993-10-02
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Abstract

Abstract Location of meteoroid impacts in space vehicles by coating the metallic interior wall of the space vehicle with a thin layer of a coating material having contrasting color to that of the vehicle interior wall and being capable of flaking or chipping off when an impacting meteoroid deforms said wall.

Inventors

  • 👤 Battista John D Di

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-09 05:52
CPC Classifications
G; G01; G01W; G01W1/00; B; B64; B64G; B64G1/00; B64G1/22; B64G1/52; B64G1/56

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 95 words
A method of locating meteoroid impacts in manned space vehicles which comprises the steps of: providing a space vehicle; coating the interior wall of the space vehicle with a layer of coating material of a preselected thickness having contrasting color to that of the vehicle interior wall said layer being of the preselected thickness so as to be capable of flaking or chipping off when an impacting meteoroid deforms said wall subjecting the space vehicle to meteoroid impact, and observing the vehicle interior wall for flaking or chipping thereby locating the point of meteoroid impact.
Claim 2
Independent Claim 95 words
A method of locating meteoroid impacts in manned space vehicles which comprises the steps of: providing a space vehicle; coating the interior wall of the space vehicle with a layer of coating material of a preselected thickness having contrasting color to that of the vehicle interior wall said layer being of the preselected thickness so as to be capable of flaking or chipping off when an impacting meteoroid deforms said wall subjecting the space vehicle to meteoroid impact, and observing the vehicle interior wall for flaking or chipping thereby locating the point of meteoroid impact.
Claim 3
Dependent Claim 18 words
The method of claim 1 wherein the step of coating is painting the interior wall with a paint.
Claim 4
Dependent Claim 21 words
The method of claim 2 wherein the step of coating is painting the interior wall with a black pigmented paint enamel.
Claim 5
Dependent Claim 23 words
The method of claim 1 wherein the step of coating is covering the interior wall with a ceramic coating composition such as porcelain.
Claim 6
Dependent Claim 30 words
The method of claim 1 wherein the space vehicle wall provided is constructed of a metal selected from the group consisting of: aluminum alloy, stainless steel and stainless steel alloy.
Claim 7
Dependent Claim 28 words
The method of claim 5 wherein the interior wall provided is aluminum and the step of coating is painting the interior wall with a black pigmented paint enamel.

References Cited (Backward Citations)

US517975A Cited
US2944250A Cited
US2976716A Cited
US3277724A Cited
US3407304A Cited
US3744320A Cited
US3793874A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-07-28 1979-01-27 1979-07-29 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-07-28 1983-01-27 1983-07-29 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-07-28 1987-01-27 1987-07-29 $7700.00 Window Closed / Lapsed

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