Manufacture of propellant compositions and propellant charges

• US 6,036,894 A
• Filed: 05/27/1983
• Issued: 03/14/2000
• Est. Priority Date: 05/28/1982
• Status: Expired due to Term

• Current Assignee: BAE Systems Land Systems Munitions and Ordnance Ltd (BAE Systems Plc)
• Original Assignee: The secretary of state for defence in her Britannic Majesty's Government of the United Kingdom of Great Britain And Northern Ireland
• Inventors: Brown, Robert James, Spickernell, Graham James, Cooke, Ernest Melville Guthrie, Treadgold, Arthur Ronald, Tucker, Bernard George
• Primary Examiner(s): Miller, Edward A.
• Application Number:
  US06/500,628
• Time in Patent Office: 6,136 Days
• Field of Search: 149/19.9, 149/19.92, 149/19.4, 264/3.1
• US Class Current: 264/3.1
• CPC Class Codes: C06B 21/0025 the ingredient being a polymer bonded explosive or thermic component
• CPC Class Codes: C06B 45/00 Compositions or products which are defined by structure or arrangement of component of product explosive charges of particular form or shape F42B1/00, F42B3/00

Abstract

This invention relates to the manufacture of composite propellants containing rubbery binders and particulate non-binder ingredients. The process consists of curing a mixture of a functionally-terminated hydro-carbon prepolymer and a cross-linking agent to form a viscoelastic first binder composition, mixing the binder with non-binder ingredients to form a plastic propellant, and rubberising at least a part of the plastic propellant by adding to it a further quantity of the cross-linking agent, provided the propellant is formed into a propellant charge while still in a plastic state. The further quantity of the cross-linking agent may be mixed in with the plastic propellant prior to forming, or applied to the surface of the plastic propellant after having been formed into a charge.

In a preferred embodiment of the invention, the prepolymer consists of an hydroxy-terminated polybutadiene having a molecular weight of about 3000 and a functionally of about 2.2, and the cross-linking agent consists of isophorone diisocyanate.

Claims

1. A process for the manufacture of a rubbery propellant charge which comprises the steps:

of forming a plastic propellant composition comprising a solid particulate propellant and a binder forming from 5% to 25% by weight of the composition, said binder comprising a prepolymer, comprising a functionally terminated hydrocarbon chain or a co-polymer thereof, of a kind capable of being chain extended by curing into a rubbery elastomeric state, said prepolymer having been partially cured by an organic cross-linking agent so as to have an apparent viscosity in the range 2,000 to 20,000 poise at 25 degrees C.;

further treating said plastic composition with a curing agent adapted to complete the cure of said binder into said rubbery state; and

prior to curing of said binder by said curing agent, forming said plastic propellant composition into a propellant charge by a dynamic forming process in which said plastic propellant composition is shaped into said propellant charge.

2. A process as in claim 1 wherein said curing agent comprises a further quantity of cross-linking agent added to the plastic propellant composition prior to the dynamic forming process to effect said further curing after said dynamic forming process.

3. A process as in claim 1 wherein said curing agent comprises a further quantity of cross-linking agent which is applied to said propellant charge after said dynamic forming process.

4. A process as in claim 3 wherein said further quantity of cross-linking agent is applied to said charge by spraying said cross-linking agent in a solvent.

5. A process as in claim 3 wherein the plastic propellant composition is deaerated in vacuo and consolidated prior to said dynamic forming process.

6. A process as in claim 1 wherein said prepolymer comprises a functionally terminated polybutadiene or a co-polymer thereof.

7. A process as in claim 1 wherein said prepolymer comprises a hydroxy terminated polybutadiene.

8. A process as in claim 2 wherein said cross-linking agent and said curing agent are both an agent which comprises an organic diisocyanate.

9. A process as in claim 8 wherein the dilsocyanate is isophorone diisocyanate and the binder of the plastic propellant composition prior to said further curing comprises from 0.5 to 0.65 equivalents of isophorone diisocyanate.

10. A process as in claim 7 wherein the hydroxy terminated polybutadiene has a functionality of from 2.0 to 3.0.

11. A process as in claim 1 wherein said plastic propellant composition is formed by partially curing said binder in the absence of said solid particulate propellant and subsequently mixing said partially cured binder with ingredients of said solid particulate propellant.

12. A process as claimed in claim 1 wherein said dynamic forming process is an extrusion process.

13. A process as in claim 1 wherein said dynamic forming process is a press-forming process.

14. A process as in claim 1 wherein said dynamic forming process is an injection molding process.

15. A process as claimed in claim 9 wherein in the further curing of the plastic propellant composition said binder comprises from 0.75 to 1.0 equivalents of isophorone diisocyanate.

16. A process according to claim 1 wherein said particular propellant comprises by weight of said rubbery propellant charge 0-10% hydrocarbon fuel, 0-24% metallic reducing agent, 0-85% oxidant of average particle size between 1 and 4 microns, 0-90% oxidant of average particle size greater than 4 microns, 0-50% coolant, and 0-2% burning rate catalyst, provided the combined weight of oxidant and coolant is 65-90% by weight of said composition.

17. A process according to claim 16 wherein said particulate ingredients comprise by weight of said rubbery propellant charge 0% hydrocarbon fuel, 0-15% metallic reducing agent, 40-80% of oxidant of average particle size from 1 to 4 microns, 0-40% oxidant of particle size greater than 4 microns but less than 50 microns, 0% coolant, and 0% burning rate catalyst, provided the overall weight of oxidant and coolant is 70-88% by weight of said rubbery composition.

18. A process according to claim 16 wherein the hydrocarbon fuel is polyethylene, the metallic reducing agent is aluminium, the oxidants are selected from the group consisting of ammonium perchlorate and ammonium nitrate, the coolant is selected from the group consisting of ammonium picrate and oxamide, and the burning rate catalyst is selected from the group consisting of cooper oxide, iron oxide, cooper chromate and chromium sesquioxide.