Insensitive munition propellants

US9919980B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9919980-B2
Application numberUS-201414780412-A
CountryUS
Kind codeB2
Filing dateMar 18, 2014
Priority dateMar 27, 2013
Publication dateMar 20, 2018
Grant dateMar 20, 2018

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The invention relates to Insensitive Munition (IM) energetic materials particularly IM propellant compositions, and yet further to nitrocellulose-free IM propellants. An energetic composition suitable for use as a propellant comprises the following components in the following relative proportions: component A; from 5% to 25% by weight of an IM energetic filler; component B: from 50% to 80% by weight of a highly energetic filler comprising at least one nitramine compound; component C of from 5% to 20% by weight of a binder; and component D of from 3% to 15% by weight of a plasticizer; the percentages by weight of components A, B, C and D together with minor additives, if any, adding to 100%.

First claim

Opening claim text (preview).

The invention claimed is: 1. An energetic non-nitrocellulose composition suitable for use as a propellant comprises the following components in the following relative proportions: component A: of from 8% to 12% by weight of an Insensitive Munition (IM) energetic filler, wherein component A is at least one of Nitrotriazolone (NTO), Hexanitrostilbene (HNS), Nitroguanidine (Picrite), and Triaminotrinitrobenzene (TATB); component B: of from 65% to 75% by weight of a highly energetic filler comprising at least one nitramine compound; component C: of from 8% to 16% by weight of a binder, wherein the binder includes a non-energetic binder; and component D: of up to 10% by weight of a plasticiser, which includes an energetic plasticiser present in the range of from 3%-8% by weight and a non-energetic plasticiser present in the range of from 2%-6% by weight, wherein the percentages by weight of components A, B, C and D together with minor additives, if any, adding to 100%. 2. An energetic composition suitable for use as a propellant comprises the following components in the following relative proportions: component A: of from 10% to 20% by weight of an Insensitive Munition (IM) energetic filler, wherein component A is at least one of Nitrotriazolone (NTO), Hexanitrostilbene (HNS), Nitroguanidine (Picrite), and Triaminotrinitrobenzene (TATB); component B: of from 55% to 70% by weight of a highly energetic filler comprising at least one nitramine compound; component C: of from 10% to 16% by weight of a binder, wherein the binder comprises a non-energetic binder and an energetic binder, and the energetic binder is present in the range of from 5-10% by weight, and the non-energetic binder is present in the range of from 5-15% by weight; and component D: of from 5% to 10% of a plasticiser, wherein the plasticiser comprises at least one of a non-energetic plasticiser and an energetic plasticiser, and the energetic plasticiser is present up to 8% by weight, and the non-energetic plasticiser is present in the range of from 2%-10% by weight, wherein the percentages by weight of components A, B, C and D together with minor additives, if any, adding to 100%. 3. A gun propellant comprising sticks or granules comprising a composition according to claim 1 . 4. An energetic composition, according to claim 2 , wherein component B comprises 65% to 70% by weight, component C comprises 8% to 12% by weight, and component D comprises an energetic plasticiser present in the range of from 3%-8% by weight and a non-energetic plasticiser present in the range of from 2%-6% by weight. 5. A gun propellant comprising sticks or granules comprising a composition according to claim 2 . 6. An energetic composition suitable for use as a propellant comprises the following components in the following relative proportions: component A: of from 5% to 25% by weight of an Insensitive Munition (IM) energetic filler selected from at least one of Nitrotriazolone (NTO), Hexanitrostilbene (HNS), Nitroguanidine (Picrite), and Triaminotrinitrobenzene (TATB); component B: of from 50% to 80% by weight of a highly energetic filler comprising at least one nitramine compound; component C: of from 5% to 20% by weight of a binder, wherein the binder comprises a mixture of a non-energetic binder and an energetic binder, with the energetic binder being present in the range of from 5-10% by weight, and the non-energetic binder being present in the range of from 5-15% by weight; and component D: of from 3% to 15% of a plasticiser, wherein the plasticiser comprises a mixture of a non-energetic plasticiser and an energetic plasticiser with the energetic plasticiser being present up to 8% by weight, and the non-energetic plasticiser being present in the range of from 2%-10% by weight, wherein the percentages by weight of components A, B, C and D together with minor additives, if any, adding to 100%. 7. A gun propellant comprising sticks or granules comprising a composition according to claim 6 . 8. An energetic composition suitable for use as a propellant comprises the following components in the following relative proportions: component A; of from 5% to 25% by weight of an IM energetic filler; component B: of from 70% to 80% by weight of a highly energetic filler comprising at least one nitramine compound; component C: of from 10% to 20% by weight of a binder comprising a mixture of a non-energetic binder present in the range of from 5-15% by weight and an energetic binder of in the range of from 5-10% by weight; and component D: of from 3% to 15% by weight of a plasticiser wherein, the plasticiser is a mixture of a non-energetic plasticiser and an energetic plasticiser, and the energetic plasticiser is present up to 8% by weight, and the non-energetic plasticiser is present in the range of from 2%-10% by weight, wherein the percentages by weight of components A, B, C and D together with minor additives, if any, adding to 100%, provided that component C is other than nitrocellulose. 9. A composition according to claim 8 , wherein: component A comprises of from 10% to 20% by weight, component B comprises of from 55% to 70% by weight, component C comprises of from 8% to 16% by weight and component D comprises of from 5% to 10% by weight of the said composition, together with any minor additives, if any, the percentages adding to 100%. 10. An energetic non-nitrocellulose composition according to claim 1 , wherein component A comprises Picrite. 11. An energetic non-nitrocellulose composition according to claim 1 , wherein component B comprises RDX. 12. An energetic non-nitrocellulose composition according to claim 1 , wherein component C comprises EVA. 13. An energetic non-nitrocellulose composition according to claim 1 , wherein component D comprises butyl NENA. 14. An energetic composition according to claim 2 , wherein component A comprises Picrite. 15. An energetic composition according to claim 2 , wherein component B comprises RDX. 16. An energetic composition according to claim 2 , wherein component C comprises EVA. 17. An energetic composition according to claim 2 , wherein component D comprises butyl NENA. 18. An energetic composition according to claim 6 , wherein component A comprises Picrite. 19. An energetic composition according to claim 6 , wherein component B comprises RDX. 20. An energetic composition according to claim 6 , wherein component C comprises EVA. 21. An energetic composition according to claim 6 , wherein component D comprises butyl NENA.

Assignees

Inventors

Classifications

  • The resin being a polymer bearing energetic groups or containing a soluble organic explosive · CPC title

  • C06B25/34Primary

    the compound being a nitrated acyclic, alicyclic or heterocyclic amine · CPC title

  • the organic component containing a resin · CPC title

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What does patent US9919980B2 cover?
The invention relates to Insensitive Munition (IM) energetic materials particularly IM propellant compositions, and yet further to nitrocellulose-free IM propellants. An energetic composition suitable for use as a propellant comprises the following components in the following relative proportions: component A; from 5% to 25% by weight of an IM energetic filler; component B: fr…
Who is the assignee on this patent?
Bae Systems Plc
What technology area does this patent fall under?
Primary CPC classification C06B25/34. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Mar 20 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).