Consolidated charges incorporating integral ignition compounds

Claim 2

In a process for consolidating a charge of nitrocellulose-based propellant grains, the improvement of incorporating an ignition compound matrix comprised of certain decahydrodecaborate compounds, through the steps of: (A) wetting loose propellant grains on their exterior surfaces with a consolidating fluid having a solvating effect on said grains, the consolidating fluid being in the range of approximately 0.010 to 0.100 milliliters of fluid per gram of propellant, and, (B) introducing a layer of decahydrodecaborate compound onto the exterior surfaces of said grains as the result of the wetting effect of said consolidating fluid, wherein said compound is in the range of approximately 0.1% to 4.0% of the total propellant weight, wherein said compound further includes a salt selected from the class of salts having the common anion B 10 H 10 -2 , and a cation selected from the group consisting of: (i) ammonium, wherein the salt has the formula (NH 4 ) 2 B 10 H 10 ; (ii) hydrazinium, wherein the salt has the general formula (NH 2 NH 3 )B 10 H 10 ; (iii) metal ions derived from the elements in Groups 1, 2, 8, 3b, 4b, 5b, 6b, 7b, and the elements of Groups 3a, 4a, 5a, and 6a which have atomic numbers respectively greater than 5, 14, 33 and 52; and (C) consolidating the thusly wetted propellant grains into a consolidated charge by a compaction step, wherein the decahydrodecaborate compound layer on each grain becomes a matrix between the grain-to-grain boundaries of the consolidated charge.

Claim 3

The process according to claim 1 wherein the decahydrodecaborate compound selected is soluble in the consolidating fluid, and the step of introducing said compound further consists of first dissolving said compound in said fluid, and wetting the exteriors of said propellant grains with the solution in order to form said layer on each grain.

Claim 4

The process according to claim 1 wherein the decahydrodecaborate compound selected is insoluble in the consolidating fluid, and the step of introducing said compound further consists of first suspending compound particles of approximately ten microns average diameter in said fluid, and wetting the exterior of said propellant grains with the suspension in order to form said layer on each grain.

Claim 5

The process according to claim 1 wherein said compound is insoluble in said fluid and is the resultant product of a coprecipitation of one of said salts with a solid oxidizing agent by the steps of: (i) dissolving both the decahydrodecaborate (-2) salt and the oxidizing agent in a mutually soluble solvent, at a temperature sufficiently high to maintain said salt and said oxidizing agent in solution; (ii) forming a pressurized stream of said solution and bringing said solution stream together with a pressurized stream of a miscible nonsolvent, under conditions of extreme turbulence within a mixing chamber, to effect a substantially complete coprecipitation; (iii) recovering the coprecipitated product by filtering the effluent from said mixing chamber, and washing said product with an inert and nonsolvent fluid; (iv) drying the product to remove all remaining liquid.

Claim 6

The process according to claim 1 wherein the step of introducing said compound further consists of first wetting the propellant grains and then tumbling the wetted grains in a powder of said compound in order to form said layer in each grain.

Claim 7

The process according to claim 1 wherein said granular nitrocellulose based propellant is selected from the group consisting of nitrocellulose, nitrocellulose/nitroglycerine, and nitrocellulose/nitroglycerine/nitroguanidine based gun propellants.

Claim 8

The process according to claim 1 wherein the consolidating fluid having a solvating effect on said propellant includes one or more members from the group consisting of: acetone, methyl ethyl ketone, methyl isobutyl ketone, methanol, ethanol, isopropanol, butyl alcohols, diacetone alcohol, butyl acetate, dibutylphthalate, ethyl ether and isopropyl ether.

Claim 9

The process according to claim 6 wherein the granular propellant selected is nitrocellulose based, said decahydrodecaborate compound selected in bisammonium decahydrodecaborate, said consolidation fluid is a mixture of approximately 65% by volume ethanol and 35% by volume acetone, and said introducing step further consists of first dissolving approximately 0.9 gram of said salt per 100 milliliter of said fluid prior to said wetting step.

Claim 10

The product of a consolidated charge according to the process of claim 8.

Claim 11

A process according to claim 4 wherein the decahydrodecaborate compound selected is a simple metallic salt selected from the group consisting of cesium decahydrodecaborate, Cs 2 B 10 H 10 , potassium decahydrodecaborate K 2 B 10 H 10 , and the simple metallic decahydrodecaborate salts of the alkaline and alkaline earth metals of Groups 1a and 2a having an atomic number less than 87.

Claim 12

In a process for consolidating a charge of nitrocellulose-based propellant grains, the improvement of incorporating an ignition compound matrix comprised of certain decahydrodecaborate compounds, through the steps of: (A) wetting loose propellant grains on their exterior surfaces with a consolidating fluid having a solvating effect on said grains, the consolidating fluid being in the range of approximately 0.010 to 0.100 milliliters of fluid per gram of propellant; and, (B) introducing a layer of decahydrodecaborate compound onto the exterior surfaces of said grains as the result of the wetting effect of said consolidating fluid, wherein said compound is in the range of approximately 0.1% to 4.0% of the total propellant weight, wherein said compound further includes a salt selected from the class of salts having the common anion B 10 H 10 -2 , and a cation selected from the group consisting of: (i) substituted ammonium cations, wherein the salt has the general formula (R 3 NH) 2 B 10 H 10 , wherein further R is selected from the group consisting of hydrogen and alkyl radicals containing less than six carbon atoms; (ii) substituted hydrazinium cations, wherein the salt has the general formula (R 2 NNR 2 H) 2 B 10 H 10 wherein further R is selected from the group consisting of hydrogen and alkyl radicals containing less than six atoms; (iii) tetramethylammonium, (CH 3 ) 4 N+, tetraethylammonium, (CH 3 CH 2 ) 4 N+, and quaternary ammonium cations having the general formula R 4 N+ where R is an alkyl radical; (iv) pyrididinium, bipyridinium aryl-diazonium, aryl containing cations and substituted aryl containing cations. (v) the guanidinium cation, C(NH 2 ) 3 +; and, (C) consolidating the thusly wetted propellant grains into a consolidated charge by a compaction step, wherein the decahydrodecaborate compound layer on each grain becomes a matrix between the grain-to-grain boundaries of the consolidated charge.

Claim 13

In a process for consolidating a charge of nitrocellulose-based propellant grains, the improvement of incorporating an ignition compound matrix comprised of certain decahydrodecaborate compounds, through the steps of: (A) wetting loose propellant grains on their exterior surfaces with a consolidating fluid having a solvating effect on said grains, the consolidating fluid being in the range of approximately 0.010 to 0.100 milliliters of fluid per gram of propellant; and, (B) introducing a layer of decahydrodecaborate compound onto the exterior surfaces of said grains as the result of the wetting effect of said consolidating fluid, wherein said compound is in the range of approximately 0.1% to 4.0% of the total propellant weight, wherein said compound further includes a salt selected from the class of salts having the common anion B 10 H 10 -2 , and a cation selected from the group consisting of: (i) substituted ammonium cations, wherein the salt has the general formula (R 3 NH) 2 B 10 H 10 , wherein further R is selected from the group consisting of hydrogen and alkyl radicals containing less than six carbon atoms; (ii) substituted hydrazinium cations, wherein the salt has the general formula (R 2 NNR 2 H) 2 B 10 H 10 wherein further R is selected from the group consisting of hydrogen and alkyl radicals containing less than six atoms; (iii) tetramethylammonium, (CH 3 ) 4 N+, tetraethylammonium, (CH 3 CH 2 ) 4 N+, and quaternary ammonium cations having the general formula R 4 N+ where R is an alkyl radical; (iv) pyrididinium, bipyridinium aryl-diazonium, aryl containing cations and substituted aryl containing cations. (v) the guanidinium cation, C(NH 2 ) 3 +; and, (C) consolidating the thusly wetted propellant grains into a consolidated charge by a compaction step, wherein the decahydrodecaborate compound layer on each grain becomes a matrix between the grain-to-grain boundaries of the consolidated charge.

Claim 14

The process according to claim 11 wherein the decahydrodecaborate compound selected is soluble in the consolidating fluid, and the step of introducing said compound further consists of first dissolving said compound in said fluid, wetting the exteriors of said propellant grains with the solution in order to form said layer on each grain.

Claim 15

The process according to claim 11 wherein the decahydrodecaborate compound selected is insoluble in the consolidating fluid, and the step of introducing said compound further consists of first suspending compound particles of approximately ten microns average diameter in said fluid, and wetting the exteriors of said propellant grains with the suspension in order to form said layer on each grain.

Claim 16

The process according to claim 11, wherein said compound is insoluble in said fluid and is the resultant product of a coprecipitation of one of said salts with a solid oxidizing agent by the steps of: (i) dissolving both the decahydrodecaborate (-2) salt and the oxidizing agent in a mutually soluble solvent, at a temperature sufficiently high to maintain said salt and said oxidizing agent in solution; (ii) forming a pressurized stream of said solution and bringing said solution stream together with a pressurized stream of a miscible nonsolvent, under conditions of extreme turbulence within a mixing chamber, to effect a substantially complete coprecipitation; (iii) recovering the coprecipitated product by filtering the effluent from said mixing chamber, and washing said product with an inert and nonsolvent fluid; (iv) drying the product to remove all remaining liquid.

Claim 17

The process according to claim 11 wherein the step of introducing said compound further consists of first wetting the propellant grains and then tumbling the wetted grains in a powder of said compound in order to form said layer on each grain.

Claim 18

The process according to claim 11 wherein said granular nitrocellulose based propellant is selected from the group consisting of nitrocellulose, nitrocellulose/nitroglycerine, and nitrocellulose/nitroglycerine/nitroguanidine based gun propellants.

Claim 19

The process according to claim 11 wherein the consolidating fluid having a solvating effect on said propellant includes one or more members from the group consisting of: acetone, methyl ethyl ketone, methyl isobutyl ketone, methanol, ethanol, isopropanol, butyl alcohols, diacetone alcohol, butyl acetate, dibutylphthalate, ethyl ether and isopropyl ether.

Claim 20

The process according to claim 14 wherein the coprecipitated decahydrodecaborate compound is approximately 15% to 25% by weight tetramethylammonium decahydrodecaborate and the remainder an oxidizing agent selected from the group consisting of ammonium nitrate, potassium nitrate, potassium perchlorate, ammonium perchlorate, guanidine nitrate, triaminoguanidine nitrate, potassium permanganate, sodium chromate, barium nitrate, barium chromate, barium manganate, sodium dichromate, tetramethylammonium nitrate and cesium nitrate, wherein further the consolidating fluid includes one or more members selected from the group consisting of isopropanol, butylacetate/ethanol, acetone/ethanol, and ether/ethanol.

Claim 21

The product of a consolidated charge according to the process of claim 18.