A resulting extended bulk explosive and the process for preparing and blending oil shale particulate with bulk explosives is provided, whereby the extending bulk explosive reduces its detonation velocity. The process includes the proper preparation of oil shale granulates to gain different cost effects and performance levels with predetermined blending percentages. The oil shale granulates may be crushed, screened, dried and prepared for blending in accordance to the disclosure of the present invention.

A primer composition is provided having a primary explosive and an oxidizer system containing at least one tungsten oxide or one tungstate compound. The oxidizer system can by non-hydroscopic and non-toxic. The primer can include reducing agents, sensitizers, binders and gas producing agents. The primer composition generally is applicable to any application or device that employs ignition of a propellant, a fuel, a relay charge, a delay charge, or a booster charge, including, but not limited to, air bag gas generator systems, signaling devices, ejection seats, small, medium or large arms ammunition primers, and the like.

A pyrotechnic composition includes a fuel, an oxidizer, flow and rate control agents and oleoresin capsicum as an irritant. The composition is useful in crowd control products. The composition contains rate control ingredients to maintain combustion at a temperature below the point of degradation of the oleoresin capsicum, balanced with a booster material to maintain combustion.

Single-walled nanotubes for use as additives in energetic materials, and methods for synthesizing such materials are described. The single-walled carbon nanotube (SWNT) additives comprise a mixture of high-purity SWNT and carbon encapsulated iron nanoparticles. The SWNT mixtures may comprise no more than 5% non-SWNT carbon, and the iron nanoparticles may be from 2-5 nm. The method of synthesizing the SWNTs may comprise a high-pressure carbon monoxide (HiPCO) process. The SWNT mixtures may be adapted for use as additives in energetic processes, such as, for example, rocket motors.

The present application discloses an improved electrically controlled propellant wherein the electrically controlled propellant comprises at least one compound selected from the group comprising organosilanes, siloxanes, and poly(dimethylsiloxane)s.

A substantially cylindrical gas-generating pyrotechnical monolithic block has a thickness no lower than 10 mm, an equivalent diameter no lower than 10 mm, and a porosity lower than 5%; and a composition, given as weight percentages, which contains, for at least 94% of the weight thereof: +77.5% to 92.5% of guanidine nitrate, +5% to 10% of basic copper nitrate, and +2.5% to 12.5% of at least one inorganic titanate with a melting temperature higher than 2100 K.

A hot-gas-generating apparatus for reacting a propellant comprises a combustion chamber, at least one injector that is arranged upstream of the combustion chamber and can be closed, on the combustion chamber side, to the propellant, electrodes being integrated in said injector, and at least one supply line for the propellant. In this context, the propellant is a monopropellant and a substantially water-free ionic solution having low vapor pressure, preferably with a residual water content of less than five percent by mass, which is capable of self-sustaining combustion at a given combustion chamber pressure, and the electrodes have at least two electrodes of opposite polarity which are suitable for electrically igniting the propellant by means of a flow of current through the propellant when this propellant flows between the opposite-polarity electrodes.

A substantially cylindrical gas-generating pyrotechnical monolithic block has a thickness no lower than 10 mm, an equivalent diameter no lower than 10 mm, and a porosity lower than 5%; and a composition, given as weight percentages, which contains, for at least 94% of the weight thereof: +77.5% to 92.5% of guanidine nitrate, +5% to 10% of basic copper nitrate, and +2.5% to 12.5% of at least one inorganic titanate with a melting temperature higher than 2100 K.

An explosive mixture compositionally comprises a powdered deuteride of an alkaline earth metal or alkali metal mixed with a catalytic mixture, wherein said catalytic mixture comprises red phosphorous powder and a transition metal powder from Period 4 or Period 5 of the Periodic table.

A reduced toxicity baseline screening smoke composition and method includes a mixture of lithium perchlorate and boron. The mixture may further include a burn rate modifier and any of an inorganic chloride coolant and a carbonate coolant. The lithium perchlorate may be in the range of 75% to 95% parts by weight. The boron may be in the range of 5% to 25% parts by weight. The any of an inorganic chloride coolant and a carbonate coolant may be in the range of 5% to 25% parts by weight. The mixture may include boron oxide.