US4911795A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of preserving a composite material cased solid propellant rocket motor
Assignee: ATK Launch Systems LLC
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Filing: 1987-08-14
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Granted: 1990-03-27
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Expires: 2007-08-14
Abstract
Abstract A solid propellant rocket motor casing fabricated from strong filament in a matrix of curable polymer known in the trade as a composite motor casing is protected against permeation therethrough over long periods of time of water vapor from the atmosphere by a thin, lightweight, metal foil barrier comprising a metal foil adhesively backed tape such as aluminum foil tape spirally wrapped over the cylindrical or regular surface areas and by a separate, lightweight, metallic shell or dome having a thickness of 0.005 to 0.008 inches adhesively bonded onto the dome ends of the composite material cased solid propellant rocket motor, each metallic shell or dome being made by the use of a plastic or other destructible mold which is first coated with metal by an ion-vapor deposition process to a thickness of less than 0.005 inches, the thickness of the coating being subsequently increased by an electro-chemical coating process after which the mold is separated from the metal shell which then is adhesively bonded to the loaded rocket motor composite casing.
Inventors
- 👤 Martin T. Olliff, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 18:26
CPC Classifications
C; C25; C25D; C25D1/00; C25D1/20; F; F02; F02K; F02K9/00; F02K9/08; F02K9/32; F02K9/34
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
293 words
A method of preserving a solid propellant rocket motor from degradation resulting from water vapor in the atmosphere, said rocket motor having a case made of composite material and formed with a dome at each of the forward and aft ends with a generally cylindrically shaped surface between said domes, said composite material case being characterized in that, over a long period of time, water vapor from the atmosphere can permeate therethrough to cause the propellant bond to the case and/or an intermediate liner between the case propellant to fail resulting in an unusable rocket motor, comprising the steps of: (a) forming a mold having a surface duplicating the shape of a dome of said case of said rocket motor, said mold being made of a material that can later be separated from a metal shell formed on said mold, that can be coated by a vapor-ionization metal deposition process, and that can withstand a metal plating bath; (b) applying a coating of metal by ion-vapor deposition to the said surface of said mold, said coating being less than half a mil thick; applying a further metal coating to the ion-vapor deposited coating on said mold to build up the combined coating thereon to a thickness in the range of five to eight mils; (d) separating the metal coating on the mold from the mold to form a free-standing metal shell; adhesively bonding a metal shell as formed by steps (a) through (d) to the dome at each of the forward and aft ends of said case to form a barrier thereat against water vapor penetration; and (f) spiral wrapping a metal foil adhesively-backed tape to the cylindrically shaped surface of said case overlapped sufficiently to prevent the passage of water vapor therethrough.
Claim 2
Independent Claim
293 words
A method of preserving a solid propellant rocket motor from degradation resulting from water vapor in the atmosphere, said rocket motor having a case made of composite material and formed with a dome at each of the forward and aft ends with a generally cylindrically shaped surface between said domes, said composite material case being characterized in that, over a long period of time, water vapor from the atmosphere can permeate therethrough to cause the propellant bond to the case and/or an intermediate liner between the case propellant to fail resulting in an unusable rocket motor, comprising the steps of: (a) forming a mold having a surface duplicating the shape of a dome of said case of said rocket motor, said mold being made of a material that can later be separated from a metal shell formed on said mold, that can be coated by a vapor-ionization metal deposition process, and that can withstand a metal plating bath; (b) applying a coating of metal by ion-vapor deposition to the said surface of said mold, said coating being less than half a mil thick; applying a further metal coating to the ion-vapor deposited coating on said mold to build up the combined coating thereon to a thickness in the range of five to eight mils; (d) separating the metal coating on the mold from the mold to form a free-standing metal shell; adhesively bonding a metal shell as formed by steps (a) through (d) to the dome at each of the forward and aft ends of said case to form a barrier thereat against water vapor penetration; and (f) spiral wrapping a metal foil adhesively-backed tape to the cylindrically shaped surface of said case overlapped sufficiently to prevent the passage of water vapor therethrough.
Claim 3
Dependent Claim
16 words
A method as defined by claim 1 wherein said mold is made of expanded bead polystyrene.
Claim 4
Dependent Claim
31 words
A method as defined by claim 2 wherein the combined metal coating formed on said expanded bead polystyrene mold is separated from the mold by dissolving the mold with a solvent.
Claim 5
Dependent Claim
17 words
A method as defined by claim 1 wherein said mold is made of a sand-polyvinyl alcohol mixture.
Claim 6
Dependent Claim
30 words
A method as defined by claim 4 wherein the combined metal coating formed said sand-polyvinyl alcohol mixture mold is separated from the mold by dissolving the mold with a solvent.
Claim 7
Dependent Claim
20 words
A method as defined by claim 1 wherein the metal coating deposited on said mold by ion-vapor deposition is aluminum.
Claim 8
Dependent Claim
20 words
A method as defined by claim 6 wherein the further metal coating applied to the ion-vapor deposited coating is aluminum.
Claim 9
Dependent Claim
23 words
A method as defined by claim 7 wherein said further metal coating is applied to the ion-vapor deposited coating by a electroplating process.
Claim 10
Dependent Claim
43 words
A method as defined by claim 8 wherein said mold is made of expanded bead polystrene, and wherein the combined metal coating formed on said expanded bead polystyrene mold is separated therefrom by dissolving the expanded bead polystyrene mold with Metyl Ethyl Ketone.
Claim 11
Dependent Claim
42 words
A method as defined in claim 8 wherein said mold is made of a sand-polyvinyl alcohol mixture, and wherein the combined metal coating formed on said sand-polyvinyl alcohol mixture mold is separated therefrom by dissolving the sand-polyvinyl alcohol mixture mold with water.
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) | 1993-03-26 | 1993-09-25 | 1994-03-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-03-26 | 1997-09-25 | 1998-03-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-03-26 | 2001-09-25 | 2002-03-27 | $7700.00 | Window Closed / Lapsed |