Ignition enhancing propellant coatings

Claim 2

A process for incorporating an ignition compound comprised of certain dechydrodecaborate compounds directly upon exterior surfaces of uncoated nitrocellulose-based propellant grains, through the steps of: (A) wetting uncoated, loose propellant grains on their exterior surfaces with a coating fluid having a solvating effect on said grains, the coating fluid being in the range of approximately 0.010 to 0.100 milliliters of fluid per gram of propellant, (B) introducing a layer of decahydrodecaborate compound onto the exterior surfaces of said grains as the result of the wetting effect of said coating 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) drying the thusly coated propellant grains until the exterior surface of each grain presents a dry appearance.

Claim 3

The process according to claim 1 wherein the decahydrodecaborate compound selected is soluble in the coating 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 coating 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

A process according to claim 1 wherein the step of drying the coated grains further comprises tumbling the wetted and coated propellant grains in a container containing fine particle graphite powder, thereafter vibrating the coated grains with the adhering graphite powder to create a glazed appearance, as the result of grain-to-grain rubbing action, and drying the glazed grains to a dry appearance.

Claim 7

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

Claim 8

The process according to claim 1 wherein the coating fluid having a solvating effect on said uncoated propellant grains 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, dibutylphthlate, ethyl ether and isopropyl ether.

Claim 9

The process according to claim 1 wherein said decahydrodecaborate compound selected is bisammonium decahydrodecaborate, said coating 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 0.125 gram of said salt per milliliter of said fluid prior to said wetting step.

Claim 10

The product of a coated granular propellant according to the process of claim 8.

Claim 11

A process according to claim 1 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 decahydrodecaborates salts of the alkaline and alkaline earth metals of Groups 1a and 2a having an atomic number less than 87.

Claim 12

The process according to claim 10 wherein said decahydrodecaborate compound selected is bispotassium decahydrodecaborate, said coating 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 0.125 gram of said salt per milliliter of said fluid prior to said wetting step.

Claim 13

The product of a coated granular propellant according to the process of claim 11.

Claim 14

A process for incorporating an ignition compound comprised of certain dechydrodecaborate compounds directly upon exterior surfaces of uncoated nitrocellulose-based propellant grains, through the steps of: (A) wetting uncoated, loose propellant grains on their exterior surfaces with a coating fluid having a solvating effect on said grains, the coating 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 coating 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 NHR 2 H) 2 B 10 H 10 wherein further R is selected from the group consisting of hydrogen and alkyl radicals contain less than six atoms; (iii) tetramethylammonium, (CH 3 ) 4 N+, tetraethylammonium, (CH 3 CH 2 ) 4 N+, and quanternary 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 (D) drying the thusly coated propellant grains until the exterior surface of each grain presents a dry appearance.

Claim 15

A process for incorporating an ignition compound comprised of certain dechydrodecaborate compounds directly upon exterior surfaces of uncoated nitrocellulose-based propellant grains, through the steps of: (A) wetting uncoated, loose propellant grains on their exterior surfaces with a coating fluid having a solvating effect on said grains, the coating 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 coating 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 NHR 2 H) 2 B 10 H 10 wherein further R is selected from the group consisting of hydrogen and alkyl radicals contain less than six atoms; (iii) tetramethylammonium, (CH 3 ) 4 N+, tetraethylammonium, (CH 3 CH 2 ) 4 N+, and quanternary 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 (D) drying the thusly coated propellant grains until the exterior surface of each grain presents a dry appearance.

Claim 16

The process according to claim 13 wherein the decahydrodecaborate compound selected is soluble in the coating 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 17

The process according to claim 13 wherein the decahydrodecaborate compound selected is insoluble in the coating 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 18

The process according to claim 13 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 19

A process according to claim 13 wherein the step of drying the coating grains further comprises tumbling the wetted and coated propellant grains in a container containing fine particle graphite powder, thereafter vibrating the coated grains with the adhering graphite powder to create a glazed appearance, as the result of grain-to-grain rubbing action, and drying the glazed grains to a dry appearance.

Claim 20

The process according to claim 13 wherein said uncoated granular nitrocellulose based propellant is selected from the group consisting of nitrocellulose, nitrocellulose/nitroglycerine and nitrocellulose/nitroglyercine/nitroguanidine based gun propellants.

Claim 21

The process according to claim 13 wherein the coating fluid having a solvating effect on said uncoated propellant grains 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, dibutylphthlate, ethyl ether and isopropyl ether.

Claim 22

The process according to claim 13 wherein said decahydrodecaborate compound selected is bisammonium decahydrodecaborate, said coating 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 0.125 gram of said salt per milliliter of said fluid prior to said wetting step.

Claim 23

The product of a coated granular propellant according to the process of claim 20.

Claim 24

The process according to claim 16 wherein the coprecipitated decahydrodecaborate compound is approximately 15 to 25% by weight ammonium 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 coating fluid includes one or more members selected from the group consisting of isopropanol, butylacetate/ethanol, acetone/ethanol, and ether/ethanol.

Claim 25

The product of a coated granular propellant according to the process of claim 22.