Explosive compositions are disclosed herein. The compositions include a diesel fuel and a vacuum gas oil. Some compositions disclosed herein include an emulsion that includes an oxidizer in a discontinuous phase and a blend of diesel fuel and vacuum gas oil in a continuous phase. Methods of manufacturing explosive compositions are also disclosed herein.

Explosive compositions are disclosed herein. The compositions include a diesel fuel and a vacuum gas oil. Some compositions disclosed herein include an emulsion that includes an oxidizer in a discontinuous phase and a blend of diesel fuel and vacuum gas oil in a continuous phase. Methods of manufacturing explosive compositions are also disclosed herein.

Pyrotechnic compositions are provided herein. The pyrotechnic composition includes potassium nitrate (KNO.sub.3), potassium perchlorate (KClO.sub.4), an inorganic fuel including boron, an organic fuel including one or more of carbon, hydrogen, and oxygen, and one or more binders. The pyrotechnic composition may have one or more of: a heat of explosion (HEX) of greater than or equal to about 5.000 J/g, a maximum flame temperature at combustion (T.sub.c) of greater than or equal to about 2,500 K (2,227° C.), and a gas yield of greater than or equal to about 15 moles/kg. Methods of preparing the pyrotechnic composition are also provided including wet granulation methods.

Pyrotechnic compositions are provided herein. The pyrotechnic composition includes potassium nitrate (KNO.sub.3), potassium perchlorate (KClO.sub.4), an inorganic fuel including boron, an organic fuel including one or more of carbon, hydrogen, and oxygen, and one or more binders. The pyrotechnic composition may have one or more of: a heat of explosion (HEX) of greater than or equal to about 5.000 J/g, a maximum flame temperature at combustion (T.sub.c) of greater than or equal to about 2,500 K (2,227° C.), and a gas yield of greater than or equal to about 15 moles/kg. Methods of preparing the pyrotechnic composition are also provided including wet granulation methods.

A gas propelled munitions anti-fouling system has a case having an open forward mouth end, a rear end, and an interior, the rear end defining a pocket that receives a primer and a passage communicating between the pocket and the interior of the case, a quantity of propellant received within the interior of the case, a quantity of anti-fouling composition received within the interior of the case, and a bullet having a rear portion inserted into the open forward mouth end of the case. The anti-fouling composition may have at least one salt and at least one acid. The acid may be anhydrous. The salt may be sodium chloride or sodium nitrate. The acid may be anhydrous citric acid. The anti-fouling composition may have at least one abrasive. The abrasive may be stannic acid. The anti-fouling composition may be 50% salt by weight and 50% acid by weight.

A gas propelled munitions anti-fouling system has a case having an open forward mouth end, a rear end, and an interior, the rear end defining a pocket that receives a primer and a passage communicating between the pocket and the interior of the case, a quantity of propellant received within the interior of the case, a quantity of anti-fouling composition received within the interior of the case, and a bullet having a rear portion inserted into the open forward mouth end of the case. The anti-fouling composition may have at least one salt and at least one acid. The acid may be anhydrous. The salt may be sodium chloride or sodium nitrate. The acid may be anhydrous citric acid. The anti-fouling composition may have at least one abrasive. The abrasive may be stannic acid. The anti-fouling composition may be 50% salt by weight and 50% acid by weight.

A solid rocket propellant includes a hydroxyl-terminated polybudadiene (HTPB) binder system having a high molecular weight diol that is greater than thirty carbon atoms (>C.sub.30) and less than fifty carbon atoms (<C.sub.50) and excluding dimeryl diisocyanate (DDI).

A solid rocket propellant includes a hydroxyl-terminated polybudadiene (HTPB) binder system having a high molecular weight diol that is greater than thirty carbon atoms (>C.sub.30) and less than fifty carbon atoms (<C.sub.50) and excluding dimeryl diisocyanate (DDI).

Explosive compositions are disclosed herein. The compositions include a diesel fuel and a vacuum gas oil. Some compositions disclosed herein include an emulsion that includes an oxidizer in a discontinuous phase and a blend of diesel fuel and vacuum gas oil in a continuous phase. Methods of manufacturing explosive compositions are also disclosed herein.

Explosive compositions are disclosed herein. The compositions include a diesel fuel and a vacuum gas oil. Some compositions disclosed herein include an emulsion that includes an oxidizer in a discontinuous phase and a blend of diesel fuel and vacuum gas oil in a continuous phase. Methods of manufacturing explosive compositions are also disclosed herein.