10results about "Non-explosive stabilisers" patented technology

A fuel composition for producing an emulsion explosive composition comprises a mixture of a liquid fuel and an emulsifying agent, wherein the emulsifying agent comprises nanoparticles in a weight % that is from about 0.05% to about 2% of the weight of the fuel composition.

The invention belongs to the technical field of stabilization of nitrate ester compounds, and particularly relates to application of poly (p-phenylenediamine) as a stabilizer for the nitrate ester compounds, and the addition amount of the poly (p-phenylenediamine) is 2.9%-3.1% on the basis of the total weight of the nitrate ester compounds. The preparation method of the poly (p-phenylenediamine) comprises the following steps: taking ammonium persulfate as an oxidizing agent, taking p-phenylenediamine as a monomer, adopting a spiral gas-solid two-phase flow technology, and enabling raw material solid particles to mutually rub and collide to initiate an oxidative polymerization reaction, so as to prepare the poly (p-phenylenediamine). The poly (p-phenylenediamine) has the characteristics of low price, easiness in synthesis, no toxicity, excellent nitrogen oxide absorption capacity and the like, has good compatibility with nitrate ester compounds, can effectively reduce the autocatalysis phenomenon and improve the long-term stability of the nitrate ester compounds, can avoid the toxicity problem of the traditional amine stabilizer when being used as the stabilizer, and has the advantages of low cost, low cost and the like. The environment and human health are facilitated.

The present disclosure provides a gas-generating agent composition, a gas-generating agent, and a preparation method and the use. The gas-generating agent composition comprises the following components, in percentages by mass: 30-70% of guanidine nitrate, 20-60% of basic copper nitrate, 0-10% of basic copper carbonate, 1-10% of ammonium perchlorate and 1-15% of a slag-forming agent, wherein the slag-forming agent comprises a first component and a second component, the first component being selected from aluminum hydroxide, and the second component being selected from at least one of a zirconate and a silicate.

The present disclosure provides for an explosive inhibitor composition which can be used to form explosive compositions comprising ammonium nitrate which are less susceptible to unwanted detonations due to the reaction between the ammonium nitrate and pyrite and / or other reactive sulphide minerals. The inhibitor composition comprises at least one component which contributes to the inhibition of this unwanted reaction and improves safety in using such explosive compositions with reactive ground.

The present invention relates to a composition in the form of a powder comprising: a polymer A which is a fluorinated polymer A1, a polyamide A2 or a polyamide-polyether block copolymer A3 or a mixture thereof; and a compound having an oxygen balance of less than 60.

The invention relates to a propellant composite for a safety device, obtainable by a method comprising the following steps: providing at least one pyrotechnic material and at least one stabilizer selected from the group consisting of monosaccharides, disaccharides, and sugar alcohols, as well as combinations thereof, wherein the at least one pyrotechnic material comprises at least one fuel and at least one oxidizing agent; and grinding the at least one pyrotechnic material and the at least one stabilizer to obtain the propellant composite. Furthermore, a method for producing the propellant composite and a propellant element are proposed.

The present invention relates to a composition in powder form comprising a polymer A, which is a fluoropolymer A1, a polyamide A2 or a polyamide-polyether block copolymer A3 or mixtures thereof, and a compound having an oxygen balance of less than 60.

The present application relates to a kind of 3-nitro-1,2,4-triazole-5-ketone / zirconium dioxide composite nano energetic material and its preparation method, the material is composed of "core" and "shell" two parts."Core" is NTO particle, and 3-nitro-1,2,4-triazole-5-ketone particle with particle size of 500-5000nm is obtained by spray drying."Shell" is nano zirconium dioxide particle with particle size of 5-300nm.3-nitro-1,2,4-triazole-5-ketone / zirconium dioxide composite nano energetic material is prepared using ultrasonic mixing effect.The composite nano energetic material prepared by the present application has high energy density of 3-nitro-1,2,4-triazole-5-ketone, conductivity of zirconium dioxide, and excellent insensitivity and strong anti-metal corrosion of composite nano material.The preparation process of this method is simple, the cost is low, nano zirconium dioxide can be uniformly coated on the energetic material 3-nitro-1,2,4-triazole-5-ketone particle, and the particle size and thickness of the composite material can be controlled, with good application prospect.

Disclosed is a stabilizer composition for rocket grade hydrogen peroxide (H2O2) which is not detrimental to the combustion performance of RDREs and not detrimental to the decomposition performance of catalyst beds while simultaneously greatly increasing the storability of H2O2 in rocket propellant management systems including but not limited to tankages and regenerative cooling combustion chambers.

The application provides a normal-temperature aluminum water metal fuel propellant and a preparation method thereof, and belongs to the technical field of solid propellants. The application uses aluminum powder as fuel, which can save the cost of propellant and improve the energy characteristics of the propellant. The application uses aluminum hydride as a fuel additive, which increases the hydrogen content in the fuel, reduces the flame temperature of the propellant, and improves the specific impulse of the propellant. The application uses perchlorate and sodium sulfate hydrate as an oxidizing agent. The sodium sulfate hydrate stores water in the form of crystal water in the propellant, which overcomes the disadvantage that the aluminum / ice propellant needs to be stored at low temperature. Under normal temperature conditions, the sodium sulfate hydrate has good stability and is not easy to decompose or lose crystal water, thereby prolonging the service life of the propellant. In the combustion process, the sodium sulfate hydrate can be dehydrated to provide an oxidizing agent for the propellant and can be decomposed to generate a working medium, thereby improving the specific impulse of the propellant.