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| Application No. | Application Title | Issue Date |
| 20110168306 | CAST EXPLOSIVE COMPOSITION The invention relates to a cast explosive composition comprising a polymer-bonded explosive and a defoaming agent, and to a process for reducing the number and/or total volume of voids in a cast explosive composition comprising the steps of: combining a polymer-bonded e... | 07/14/2011 |
| 20090008001 | Extrudable gas generant Extrudable gas generant compositions which, upon combustion, produce or result in an improved effluent and related methods for generating inflation gas for use in an inflatable restraint system are provided. Such extrudable gas generant compositions include a non-azide,... | 01/08/2009 |
| 20070089817 | METHOD FOR PROVIDING GAS TO A PROCESSING CHAMBER A method and apparatus for generating gas for a processing system is provided. In one embodiment, an apparatus for generating gas for a processing system includes a canister having at least one baffle disposed between two ports and containing a precursor material. The p... | 04/26/2007 |
| 20060272754 | Propellant composition and methods of preparation and use thereof The invention relates to propellant compositions comprising a solid inorganic perchlorate oxidizing agent, a nitrogen-containing fuel, and a burn rate catalyst. Such compositions may be used as a propellant material, (e.g., in rocketry), a pyrotechnic material, an explo... | 12/07/2006 |
| 20060011277 | Pyrotechnic charge A pyrotechnic charge for producing IR radiation, in which a deuterated compound is contained as fuel and/or as oxidizing agent or as fuel, as oxidizing agent and/or as binder. The use of such a pyrotechnic charge leads to a greater selective radiant emission in the β-b... | 01/19/2006 |
| 20050189051 | Method for producing cryogenic, solid monopropellants and solid propellants produced according to said method The invention relates to a method for producing (cryogenic) solid monopropellants which are cooled to below room temperature and are used for rocket drives, especially using heterogeneous liquid-solid propellants wherein at least one of the reactants in the form of an o... | 09/01/2005 |
