The conformable pyrolant includes a fluorocarbon liquid, a fluorocarbon powder, and a micron size powdered aluminum bound together with a binder system that includes polyisobutylene and colloidal silicon dioxide. The conformable pyrolant is capable of achieving temperatures on the order 10,000 F., which will breach an ordnance item and thermally decompose an insensitive explosive fill. The conformable pyrolant also includes tungsten, wherein tungsten and silicon dioxide oxidize into fluorinated compounds, therein extending the burn and gasifying, therein enhancing ebullition and volume in general. The versatile conformable format is capable of being shaped into geometries for inclusion in ordnance items or molded into configurations for disposal of insensitive munitions.

The present disclosure relates to three-dimensional (3D) printed fluoropolymer-based energetic compositions and 3D printing methods for making the 3D printed fluoropolymer-based energetic compositions.

The present disclosure relates to three-dimensional (3D) printed fluoropolymer-based energetic compositions and 3D printing methods for making the 3D printed fluoropolymer-based energetic compositions.

Microwave energy is used to ignite and control the ignition of electrically operated propellant to produce high-pressure gas. The propellant includes conductive particles that act as a free source of electrons. Incoming microwave energy accumulates electric charge in an attenuation zone, which is discharged in the form of dielectric breakdowns to create local randomly oriented currents. The propellant also includes polar molecules. The polar molecules in the attenuation zone absorb microwave energy causing the molecules to rapidly vibrate thereby increasing the temperature of the propellant. The increase in temperature and the local current densities together establish an ignition condition to ignite and sustain ignition of an ignition surface of the attenuation zone as the zone regresses without igniting the remaining bulk of the propellant.

Microwave energy is used to ignite and control the ignition of electrically operated propellant to produce high-pressure gas. The propellant includes conductive particles that act as a free source of electrons. Incoming microwave energy accumulates electric charge in an attenuation zone, which is discharged in the form of dielectric breakdowns to create local randomly oriented currents. The propellant also includes polar molecules. The polar molecules in the attenuation zone absorb microwave energy causing the molecules to rapidly vibrate thereby increasing the temperature of the propellant. The increase in temperature and the local current densities together establish an ignition condition to ignite and sustain ignition of an ignition surface of the attenuation zone as the zone regresses without igniting the remaining bulk of the propellant.

An energetic composite comprises a metal powder; poly(vinylidene fluoride) (PVDF); and poly(lactic acid) (PLA). The metal powder comprises micrometer- or nanometer-sized particles, and the ratio of PVDF to PLA is between about 1:3 to 3:1. The metal powder comprises between about 4-32% wt of the energetic composite, and the metal powder consists of aluminum (Al), magnesium (Mg), or boron (B). A method of making an energetic composite material, comprises melt-blending a metal powder with poly(vinylidene fluoride) (PVDF) and poly(lactic acid) (PLA).

An energetic composite comprises a metal powder; poly(vinylidene fluoride) (PVDF); and poly(lactic acid) (PLA). The metal powder comprises micrometer- or nanometer-sized particles, and the ratio of PVDF to PLA is between about 1:3 to 3:1. The metal powder comprises between about 4-32% wt of the energetic composite, and the metal powder consists of aluminum (Al), magnesium (Mg), or boron (B). A method of making an energetic composite material, comprises melt-blending a metal powder with poly(vinylidene fluoride) (PVDF) and poly(lactic acid) (PLA).

A technique for forming an energetic ink is provided. The technique includes forming a non-reactive layer by disposing a composite ink on a substrate, the composite ink including a polymer binder that is solvent-permeable and porous fuel particles (e.g. porous silicon particles). Mixing, printing, casting, assembling, or otherwise handling the inert composite can occur while it remains non-reactive. Subsequently, the technique can then include depositing a liquid solution of solid oxidizer onto the non-reactive layer, which can permeate the binder and impregnate the porous fuel particles with a solid oxidizer, activating the composite ink. In this manner, components with the composite ink can be partially and safely fabricated/assembled while the ink is inert, and the ink can then be activated at a later point in a manufacturing process.

A technique for forming an energetic ink is provided. The technique includes forming a non-reactive layer by disposing a composite ink on a substrate, the composite ink including a polymer binder that is solvent-permeable and porous fuel particles (e.g. porous silicon particles). Mixing, printing, casting, assembling, or otherwise handling the inert composite can occur while it remains non-reactive. Subsequently, the technique can then include depositing a liquid solution of solid oxidizer onto the non-reactive layer, which can permeate the binder and impregnate the porous fuel particles with a solid oxidizer, activating the composite ink. In this manner, components with the composite ink can be partially and safely fabricated/assembled while the ink is inert, and the ink can then be activated at a later point in a manufacturing process.

Flares with consumable weights connected to a forward end of the grain of the flare are disclosed. Also disclosed are consumable weight components for flares. The consumable weight components include a metal material within a matrix. Also disclosed are methods for fabricating a flare and methods for using a flare. Use of the consumable weights in the flares may reduce the amount of debris falling to ground.