The invention relates to a pyrotechnic gas generator component including an inlet stage formed by a pyrotechnic detonator composition and an intermediate stage disposed between the inlet stage and an outlet stage formed by at least one gas generator composition, said intermediate stage being formed by a compressed black powder layer.

A micro-explosive material is provided. The micro-explosive material can include a carbon nanotube and a solid oxidizer attached to the carbon nanotube. The carbon nanotube with the solid oxidizer attached thereto is operable to burn per an exothermic chemical reaction between the carbon nanotube and the solid oxidizer such that a controlled burn and/or an explosive burn is provided. The micro-explosive material can be used as a heat generator, a gas generator, a micro-thruster, a primer for use with a larger explosive material, and the like.

A micro-explosive material is provided. The micro-explosive material can include a carbon nanotube and a solid oxidizer attached to the carbon nanotube. The carbon nanotube with the solid oxidizer attached thereto is operable to burn per an exothermic chemical reaction between the carbon nanotube and the solid oxidizer such that a controlled burn and/or an explosive burn is provided. The micro-explosive material can be used as a heat generator, a gas generator, a micro-thruster, a primer for use with a larger explosive material, and the like.

A method for improving the characteristics of energetic materials uses amorphous metals as one or more reactant of said materials. Improvements in properties and energy release characteristics for a wide range of energetic materials are obtained thereby, particularly in terms of processability, mechanical properties, and ignition behavior for solid energetic materials.

This invention relates to a thermal hydrogen generator and a process and system for generating hydrogen gas, more specifically to a process and system for generating hydrogen gas by thermally decomposing a metal hydride.

A projectile including a reactive composition is disclosed. The reactive composition includes at least one fuel comprising a titanium-boron composite, at least one oxidizer, and at least one metal hydride. When the projectile penetrates through a surface of a target having a volume of 0.2 m.sup.3, the reactive composition is configured to cause, behind the surface of the target, at least one of an overpressure of greater than 36 pounds per square inch (psi) or an incendiary effect duration of greater than 70 milliseconds. The reactive composition may be configured to partially or entirely surround a pin or penetrator. The projectile may lack a pin or penetrator, and the reactive composition is contained within a metal tube or cup configured to travel toward, within, and/or behind a surface of the target, wherein the process produces a punch out from the target, thereby acting as a second projectile, which enhances lethality.

A projectile including a reactive composition is disclosed. The reactive composition includes at least one fuel comprising a titanium-boron composite, at least one oxidizer, and at least one metal hydride. When the projectile penetrates through a surface of a target having a volume of 0.2 m.sup.3, the reactive composition is configured to cause, behind the surface of the target, at least one of an overpressure of greater than 36 pounds per square inch (psi) or an incendiary effect duration of greater than 70 milliseconds. The reactive composition may be configured to partially or entirely surround a pin or penetrator. The projectile may lack a pin or penetrator, and the reactive composition is contained within a metal tube or cup configured to travel toward, within, and/or behind a surface of the target, wherein the process produces a punch out from the target, thereby acting as a second projectile, which enhances lethality.

An infused solid polymeric fuel for use in a hybrid rocket or as explosive ordnance. An infused solid polymeric fuel can include a porous polymeric body having continuous pores distributed throughout a volume of the polymeric body and connecting to an external surface of the polymeric body. A combustion enhancement agent can be infused into the polymeric body. The combustion enhancement agent can be deposited on interior surfaces of the pores and on the external surface of the polymeric body. The combustion enhancement agent can include a catalyst, an oxidizer, a hypergolic fuel, or a combination.

The invention is directed to a radiation curable energetic composition, to a method of forming a three-dimensional energetic object, to a three-dimensional energetic object, and to uses of the radiation curable energetic composition. The radiation curable energetic composition of the invention comprises (a) one or more polymerisable components, (b) one or more polymerisation initiators, and (c) one or more energetic components.

The invention is directed to a radiation curable energetic composition, to a method of forming a three-dimensional energetic object, to a three-dimensional energetic object, and to uses of the radiation curable energetic composition. The radiation curable energetic composition of the invention comprises (a) one or more polymerisable components, (b) one or more polymerisation initiators, and (c) one or more energetic components.