US4009231A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Powder barrier bonding technique
Assignee: United States Department of the Navy
•
Filing: 1975-03-20
•
Granted: 1977-02-22
•
Expires: 1995-03-20
Abstract
Abstract A barrier layer made up of a suitable powder interspersed within either a trix of cured propellant binder or a matrix of silicone rubber is interposed between a silicone rubber insulator and a solid propellant grain in a rocket motor to prevent curatives from migrating from the propellant into the silicone rubber layer when the propellant is cast.
Inventors
- 👤 Bernard Wasserman
- 👤 William H. Thielbahr
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 11:24
CPC Classifications
C; C06; C06B; C06B21/00; C06B21/0083; C06B45/00; C06B45/12
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
73 words
In a method for loading a rocket motor which comprises casting and curing a solid propellant within a combustion chamber which is lined with a layer of cured silicone rubber insulator material, the improvement residing in casting and curing a barrier layer on said layer of insulator material before casting and curing the propellant grain to prevent materials in the propellant grain from migrating into the insulator layer as the propellant grain cures.
Claim 2
Dependent Claim
73 words
In a method for loading a rocket motor which comprises casting and curing a solid propellant within a combustion chamber which is lined with a layer of cured silicone rubber insulator material, the improvement residing in casting and curing a barrier layer on said layer of insulator material before casting and curing the propellant grain to prevent materials in the propellant grain from migrating into the insulator layer as the propellant grain cures.
Claim 3
Dependent Claim
51 words
In a method according to claim 1 the additional improvement residing in utilizing, as said barrier layer, a composite made up of a powder selected from the group consisting of copper, silica and aluminum interspersed in a matrix of binder selected from the group consisting of carboxy and hydroxy terminated polybutadiene.
Claim 4
Dependent Claim
19 words
A method according to claim 2 wherein the powder is silica powder and the matrix is carboxy terminated polybutadiene.
Claim 5
Dependent Claim
35 words
A method according to claim 3 wherein from 65 to 75 weight percent of the barrier layer is silica and wherein from 35 to 25 weight percent of the barrier layer is carboxy terminated polybutadiene.
Claim 6
Independent Claim
51 words
A method for providing a barrier layer to substantially prevent migration of a curing agent from a solid propellant grain into an insulation layer comprising the steps of: 1. applying an uncured blend of silicone rubber and a powder onto the cured insulation; and 2. allowing said barrier layer to cure.
Claim 7
Independent Claim
51 words
A method for providing a barrier layer to substantially prevent migration of a curing agent from a solid propellant grain into an insulation layer comprising the steps of: 1. applying an uncured blend of silicone rubber and a powder onto the cured insulation; and 2. allowing said barrier layer to cure.
Claim 8
Dependent Claim
34 words
A method according to claim 5 wherein said insulation layer is made up of silicone rubber and wherein said powder is selected from the group consisting of copper powder, silica powder and aluminum powder.
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) | 1980-02-22 | 1980-08-23 | 1981-02-22 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-02-22 | 1984-08-23 | 1985-02-22 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-02-22 | 1988-08-23 | 1989-02-22 | $7700.00 | Window Closed / Lapsed |