US4131051A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Process for preparing a rocket motor
Assignee: Olin Corp
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Filing: 1964-05-21
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Granted: 1978-12-26
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Expires: 1984-05-21
Abstract
Abstract 1. In the process for preparing a rocket motor, the improvement which comprises applying a layer of an uncured organic material capable of being cured to a rubbery material, to the interior combustion chamber wall of a rocket vessel, partially embedding powder grains in the exposed surface of said uncured material before solidification, thereafter curing and solidifying said uncured material, whereby a rubber-base liner is formed having one surface firmly adhering to said wall and said powder grains firmly adhering to the exposed surfaces of said liner, with a portion of each powder grain protruding from said liner, filling the lined portion of the chamber with a thermoplastic propellant charge, and solidifying said propellant charge, whereby a firmly adhering bond is formed between the solidified propellant charge, the powder grains and the solidified liner.
Inventors
- 👤 Otto G. Schaffling
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 00:08
CPC Classifications
F; F02; F02K; F02K9/00; F02K9/08; F02K9/32; F02K9/34; F02K9/346
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
133 words
In the process for preparing a rocket motor, the improvement which comprises applying a layer of an uncured organic material capable of being cured to a rubbery material, to the interior combustion chamber wall of a rocket vessel, partially embedding powder grains in the exposed surface of said uncured material before solidification, thereafter curing and solidifying said uncured material, whereby a rubberbase liner is formed having one surface firmly adherng to said wall and said powder grains firmly adhering to the exposed surfaces of said liner with a portion of each powder grain protruding from said liner, filling the lined portion of the chamber with a thermoplastic propellant charge, and solidifying said propellant charge, whereby a firmly adhering bond is formed between the solidified propellant charge, the powder grains and the solidified liner.
Claim 2
Dependent Claim
133 words
In the process for preparing a rocket motor, the improvement which comprises applying a layer of an uncured organic material capable of being cured to a rubbery material, to the interior combustion chamber wall of a rocket vessel, partially embedding powder grains in the exposed surface of said uncured material before solidification, thereafter curing and solidifying said uncured material, whereby a rubberbase liner is formed having one surface firmly adherng to said wall and said powder grains firmly adhering to the exposed surfaces of said liner with a portion of each powder grain protruding from said liner, filling the lined portion of the chamber with a thermoplastic propellant charge, and solidifying said propellant charge, whereby a firmly adhering bond is formed between the solidified propellant charge, the powder grains and the solidified liner.
Claim 3
Dependent Claim
19 words
The process of claim 1 wherein said powder grains have a diameter between about 0.01 and about 0.2 inches.
Claim 4
Dependent Claim
31 words
The process of claim 1 wherein the amount of said powder grains is sufficient to cover between about 50 and about 95 percent of the exposed area of said uncured material.
Claim 5
Dependent Claim
28 words
The process of claim 1 wherein said uncured organic material is a mixture of an epoxy resin, a copolymer of butadiene and acrylic acid, and a curing agent.
Claim 6
Dependent Claim
13 words
The process of claim 1 wherein said powder grains are nitrocellulose powder grins.
Claim 7
Dependent Claim
25 words
The process of claim 1 wherein said uncured organic material contains between about 2.5 and about 30 percent by weight of an inorgaic metal salt.
Claim 8
Dependent Claim
12 words
The process of claim 6 wherein said metal salt is zinc chromate.
Claim 9
Dependent Claim
67 words
The process of claim 1 wherein said uncured organic material is a mixture of an epoxy resin, a copolymr of butadiene and acrylic acid, a curing agent, and zinc chromate in a proportion equivalent to between about 2.5 and about 30 percent by weight of said mixture, and wherein said powder grains are nitrocellulose powder grains having an average diameter between about 0.01 and about 0.20 inches.
Claim 10
Dependent Claim
38 words
The process of claim 1 wherein said uncured organic material is admixed with a solvent therefore, the resulting solution is sprayed onto the interior combustion chamber wall, and the solvent is evaporated prior to applying the powder grains.
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) | 1981-12-25 | 1982-06-26 | 1982-12-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-12-25 | 1986-06-26 | 1986-12-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-12-25 | 1990-06-26 | 1990-12-26 | $7700.00 | Window Closed / Lapsed |