Crosslinked smokeless propellants

Claim 2

A smokeless crosslinked double-base propellant comprising by weight (a) from about 7% to about 17.0% nitrocellulose, (b) from about 27% to about 63% energetic plasticizer, (c) from about 4% to about 12% of a crosslinking agent which is a prepolymer prepared by reaction of a hydroxy-terminated polyester and a diisocyanate, (d) from about 0% to about 8% non-energetic plasticizer, (e) from about 0.5% to about 6% of lead salt, (f) from about 0.1% to about 0.9% carbon black, and (g) from about 0% to about 60% of oxidizer comprising cyclotrimethylene trinitramine, cyclotetramethylene tetranitramine, and mixtures thereof.

Claim 3

The smokeless crosslinked double-base propellant of claim 1 wherein the crosslinking agent is a prepolymer of polygylcol adipate and tolylene 2,4-diisocyanate.

Claim 4

The smokeless crosslinked double-base propellant of claim 2 wherein the energetic plasticizer is nitroglycerin.

Claim 5

The smokeless crosslinked double-base propellant of claim 3 wherein the non-energetic plasticizer is di-n-propyladipate.

Claim 6

The smokeless crosslinked double-base propellant of claim 4 wherein the weight ratio of nitrocellulose to the prepolymer of polyglycol adipate-tolylene 2,4-diisocyanate is from about 1.8/1.0 to about 0.7/1.0.

Claim 7

The smokeless crosslinked double-base propellant of claim 5 wherein the weight ratio of total plasticizer to nitrocellulose is from about 4.2/1.0 to about 6.6/1.0.

Claim 8

A smokeless crosslinked double-base propellant comprising by weight: (a) from about 7% to about 15% nitrocellulose, (b) from about 34% to about 56% nitroglycerin, (c) from about 4% to about 10% of a prepolymer consisting essentially of the reaction product of polyglycol adipate and tolylene 2,4-diisocyanate, said prepolymer having a molecular weight range of from about 1000 to about 2000 and an average NCO content from about 3% to about 7% by weight, based on the weight of the prepolymer, (d) from about 0% to about 5% of di-n-propyl-adipate, (e) from about 2% to about 4% of lead salts selected from the groups consisting of lead salicylate, lead beta-resorcylate and mixtures thereof, (f) from about 0.2% to about 0.5% carbon black, and (g) from about 10% to about 40% of organic oxidizer selected from the group consisting of cyclotrimethylene trinitramine, cyclotetramethylene tetranitramine, and mixtures thereof.

Claim 9

A smokeless crosslinked double-base propellant comprising by weight: (a) from about 7% to about 15% nitrocellulose, (b) from about 34% to about 56% nitroglycerin, (c) from about 4% to about 10% of a prepolymer consisting essentially of the reaction product of polyglycol adipate and tolylene 2,4-diisocyanate, said prepolymer having a molecular weight range of from about 1000 to about 2000 and an average NCO content from about 3% to about 7% by weight, based on the weight of the prepolymer, (d) from about 0% to about 5% of di-n-propyl-adipate, (e) from about 2% to about 4% of lead salts selected from the groups consisting of lead salicylate, lead beta-resorcylate and mixtures thereof, (f) from about 0.2% to about 0.5% carbon black, and (g) from about 10% to about 40% of organic oxidizer selected from the group consisting of cyclotrimethylene trinitramine, cyclotetramethylene tetranitramine, and mixtures thereof.

Claim 12

The method of claim 8 wherein the weight ratio of inert liquid to lead salt is at least about 1.2/1.0.

Claim 13

The method of claim 9 wherein the propellant is cured at 125° F. or above for at least 10 days.

Claim 14

The method of claim 8 wherein the inert liquid is a non-energetic plasticizer for nitrocellulose.

Claim 15

The method of claim 11 wherein the inert liquid is a material selected from the group consisting of di-n-propyladipate, triacetin, tri-n-butyl phosphate, dimethyl phthalate, and mixtures thereof.

Claim 16

The process of claim 8 wherein the inert liquid is a liquid selected from the group consisting of heptane, benzene and ethyl acetate.