Abstract: An energetic material device is disclosed. The energetic material device can include a casing. The energetic material device can also include an energetic material in a solid state within the casing. In addition, the energetic material device can include an optical sensor encased within the energetic material to sense a condition of the energetic material. An energetic material monitoring system is also disclosed. The energetic material monitoring system can include an energetic material device. The energetic material device can include a casing. The energetic material device can also include an energetic material in a solid state within the casing. In addition, the energetic material device can include an optical sensor encased within the energetic material. The energetic material monitoring system can also include an interrogator in communication with the optical sensor via an optical fiber.

Abstract: An energetic material device is disclosed. The energetic material device can include a casing. The energetic material device can also include an energetic material in a solid state within the casing. In addition, the energetic material device can include an optical sensor encased within the energetic material to sense a condition of the energetic material. An energetic material monitoring system is also disclosed. The energetic material monitoring system can include an energetic material device. The energetic material device can include a casing. The energetic material device can also include an energetic material in a solid state within the casing. In addition, the energetic material device can include an optical sensor encased within the energetic material. The energetic material monitoring system can also include an interrogator in communication with the optical sensor via an optical fiber.

Abstract: A non-destructive testing system for propellant for a rocket is provided. The system includes an insertion tube having a first end and a second end in addition to a support sleeve configured to mate with a casing of the rocket. The insertion tube includes a channel that extends from the first end to the second end of the insertion tube to receive a probe and also includes a probe tip generally disposed at the second end of the channel. The support sleeve includes an insertion tube opening configured to receive the insertion tube and allow the insertion tube to slide along the support sleeve.

Abstract: A non-destructive testing system for propellant for a rocket is provided. The system includes an insertion tube having a first end and a second end in addition to a support sleeve configured to mate with a casing of the rocket. The insertion tube includes a channel that extends from the first end to the second end of the insertion tube to receive a probe and also includes a probe tip generally disposed at the second end of the channel. The support sleeve includes an insertion tube opening configured to receive the insertion tube and allow the insertion tube to slide along the support sleeve.

Abstract: Improved liners and explosive devices having improved liners are provided. In accordance with an exemplary embodiment, a liner for an explosive device comprises a plate configured to be positioned against an explosive charge. The plate comprises rhenium, palladium, or a combination thereof, at least a bimodal particle size distribution having a powder grain size no greater than 25 microns, a substantially circular diameter, and a substantially concave interior relative to a surface of the explosive charge.

Abstract: Insensitive munition-type explosive material and methods for forming insensitive munition-type explosive material are provided. In an exemplary embodiment, an insensitive munition-type explosive material comprises a particle of BNCP and a surfactant-comprising shell that encapsulates the particle of BNCP.

Abstract: Explosive devices, and in particular cluster explosively-formed penetrator warhead devices, are described herein. In accordance with an exemplary embodiment, a spherically-shaped explosive device comprises an initiator, a fuze component system configured to ignite the initiator, and a substantially spherical explosive charge surrounding the initiator. The substantially spherical explosive charge has a substantially spherical surface. A plurality of liners are on the substantially spherical surface of the substantially spherical explosive charge.

Abstract: Explosive devices, and in particular cluster explosively-formed penetrator warhead devices, are described herein. In accordance with an exemplary embodiment, a spherically-shaped explosive device comprises an initiator, a fuze component system configured to ignite the initiator, and a substantially spherical explosive charge surrounding the initiator. The substantially spherical explosive charge has a substantially spherical surface. A plurality of liners are on the substantially spherical surface of the substantially spherical explosive charge.

Abstract: Improved liners and explosive devices having improved liners are provided. In accordance with an exemplary embodiment, a liner for an explosive device comprises a plate configured to be positioned against an explosive charge. The plate comprises rhenium, palladium, or a combination thereof, at least a bimodal particle size distribution having a powder grain size no greater than 25 microns, a substantially circular diameter, and a substantially concave interior relative to a surface of the explosive charge.

Abstract: Insensitive munition-type explosive material and methods for forming insensitive munition-type explosive material are provided. In an exemplary embodiment, an insensitive munition-type explosive material comprises a particle of BNCP and a surfactant-comprising shell that encapsulates the particle of BNCP.

Abstract: PBX compositions and methods for fabricating PBX compositions are provided. In an exemplary embodiment, a PBX composition comprises a binder matrix comprising a thermoset resin and an oxidizer comprising octanitrocubane (ONC), the oxidizer homogeneously dispersed within the binder matrix. In another embodiment, a method for fabricating a PBX composition comprises providing an oxidizer comprising octanitrocubane (ONC) and blending the oxidizer with a prepolymer that, upon cure, forms a thermoset resin.

Abstract: PBX compositions and methods for fabricating PBX compositions are provided. In an exemplary embodiment, a PBX composition comprises a binder matrix comprising a thermoset resin and an oxidizer comprising octanitrocubane (ONC), the oxidizer homogeneously dispersed within the binder matrix. In another embodiment, a method for fabricating a PBX composition comprises providing an oxidizer comprising octanitrocubane (ONC) and blending the oxidizer with a prepolymer that, upon cure, forms a thermoset resin.

Abstract: The inventions provide nanocrystallites and processes for the production of these nanocrystallites according to known silica-based sol-gel preparation principles based on hydrolysis/condensation mechanisms. The processes include a synthesis step comprising providing a homogenized colloidal dispersion of precursors, catalyst, and surfactant to form the sol matrix. The processes further include a novel drying step for a wet hydrogel intermediate product, including a short-cycle drying period during which the liquids present in this hydrogel can be evaporated at ambient pressure and low temperature ranges in any convenient drying apparatus while, inter alia, preserving the gel structure, especially gel porosity. Porosity values for the dried product up to about 98-99% can be attained, with product He densities as low as about 0.033 g/cc. Nanocrystallites produced by this process have, inter alia, excellent clarity, thermal insulation, acoustic insulation, surface scattering, and bulk modulus properties.

Abstract: A cylindrical, oval or egg-shaped shell comprising a plurality of layers of wood laminate with a layer of adhesive located between each adjacent layers of wood laminate. The adhesive is a composite adhesive which has a plurality of hollow spheres intermixed within the composite adhesive to facilitate improving bonding between adjacent layers of the wood laminate. The coating of the hollow spheres is preferably silane. The laminated wood core or shell has improved strength and sound qualities and is also suitable for use in the manufacture of furniture.

Abstract: This invention relates to a gas generator having two or more compartments, each with a separate initiator, with one compartment discharging before another, i.e., the compartments discharge sequentially. Each compartment has the same propellants, but the propellants have different geometries in each compartment, which results in different rates of gas evolution from each compartment. The gas generator has a rapid initial inflation, followed by a more gradual inflation rate in the subsequent stages, improving safety to occupants. One propellant used for the gas generator comprises (1) ammonium nitrate as the oxidizer, (2) a fuel such as CL-20. and (3) a binder such as polycaprolactone. A second propellant comprises by weight approximately 70-95% energetic nitrate fuel, 5-25% energetic polymer binder and 0.1-5% flash suppressant. No hot metal particles (e.g., CuO) are generated in the new systems.

Abstract: This invention relates to a gas generator having two or more compartments, each with a separate initiator, with one compartment discharging before another, i.e., the compartments discharge sequentially. Each compartment has the same propellants, but the propellants have different geometries in each compartment, which results in different rates of gas evolution from each compartment. The new gas generator is designed to reach maximum inflation at the same time as the current, single stage gas generators. However, the new generator has a more rapid initial inflation, followed by a more gradual inflation rate in the subsequent stages, improving safety to occupants. The propellant used in new generator comprises (1) ammonium nitrate as the oxidizer, which is less toxic and corrosive than the currently-used azide, (2) a fuel such as CL-20, and (3) a binder such as polycaprolactone. No hot metal particles (e.g., CuO) are generated in the new system.

Abstract: A thermal battery is housed in a chamber that utilizes micro-electromechanical systems (MEMS)-based technology to offer superior chemical stability and advantageous mechanical and thermal properties. The thermal battery of the present invention is activated by heat, for example heat generated by a pyrotechnic charge, for example thermite, for immediate and thorough activation of the electrolyte. The anode, cathode and electrolyte of the battery are formed of pellets having a curved interface for increased current density. The electrolyte preferably comprises a three-component eutectic salt mixture. In this manner, the thermal battery of the present invention is well suited for applications that require highly integrated thermal batteries that are relatively small in physical size, yet are capable of reliable performance over a wide range of operating conditions.

Abstract: A high-precision pyrotechnic initiator is well adapted for rapid, precise ignition of solid and liquid energetics. A rigid housing, for example formed of an SiC-treated semiconductor substrate material, contains a pyrotechnic. When ignited, the reaction, or explosion, of the pyrotechnic is confined to the housing. The release of energy creates a hot particulate in which the formation of solid byproducts is mitigated or eliminated. The flame is directed through an outlet. In one embodiment, a microcapillary tube may be placed in communication with the outlet, the tube including a primary front vent and secondary side vents, which serve to increase system efficiency and reliability. A dual bridge wire may be provided for improving system reliability. The resulting assembly thereby performs the combined functions of both an igniter and a flash tube and a complete ignition train is provided in a manner that overcomes the limitations of the conventional configurations.

Abstract: This invention relates to a gas generator having two or more compartments, each with a separate initiator, with one compartment discharging before another, i.e., the compartments discharge sequentially. Each compartment has the same propellants, but the propellants have different geometries in each compartment, which results in different rates of gas evolution from each compartment.

Abstract: This invention relates to a gas generator having two or more compartments, each with a separate initiator, with one compartment discharging before another, i.e., the compartments discharge sequentially. Each compartment has the same propellants, but the propellants have different geometries in each compartment, which results in different rates of gas evolution from each compartment. The new gas generator is designed to reach maximum inflation at the same time as the current, single stage gas generators. However, the new generator has a more rapid initial inflation, followed by a more gradual inflation rate in the subsequent stages, improving safety to occupants.