METHOD OF MANUFACTURING A CONSOLIDATED DOUBLE BASE PROPELLANT
First Claim
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2. The method of claim 1 wherein said reinforcing mesh has strand diameters of about 0.010-0.012 and said mesh is consolidated with a single sheet of cured double base propellant to yield said consolidated double base propellant system with a thickness up to about 0.025 inch.
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Abstract
A method is disclosed for consolidating one or more sheets of double base propellant with a reinforcing mesh to yield a consolidated propellant system.
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3 Claims
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2. The method of claim 1 wherein said reinforcing mesh has strand diameters of about 0.010-0.012 and said mesh is consolidated with a single sheet of cured double base propellant to yield said consolidated double base propellant system with a thickness up to about 0.025 inch.
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3. The method of claim 1 wherein said reinforcing mesh is consolidated with a sheet of cured double base on each side of the mesh to yield said consolidated double base propellant system.
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Current AssigneeJohn C. Horvath, Thomas E. Martin
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Original AssigneeJohn C. Horvath, Thomas E. Martin
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InventorsMartin, Thomas E., Horvath, John C.
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Primary Examiner(s)Lechert, Jr., Stephen J.
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Application NumberUS05/354,553Time in Patent Office630 DaysField of Search149/14,15 264/3AUS Class Current264/3.2CPC Class CodesC06B 45/12 having contiguous layers or...F42B 5/16 characterised by compositio...
