Patent
Conductance method for determining the mechanical properties of propellants
TLDR
In this article, a solid propellant grain is converted from a nonconductive filled elasto into a highly-conductive fill elastomer by introducing an effective amount of an alkali metal tungstate or the analogous ammonium salt which, in addition to imparting electrical conductance characteristics, also functions as an oxidizer in the propellant composition.Abstract:
A solid propellant grain is converted from a non-conductive filled elasto into a highly-conductive filled elastomer by introducing an effective amount of an alkali metal tungstate or the analogous ammonium salt which, in addition to imparting electrical conductance characteristics, also functions as an oxidizer in the propellant composition. When sodium tungstates, known as tungsten bronzes, or the analogous ammonium salt, are used to replace from 1 to 3 parts of the ammonium perchlorate oxidizer in the propellant formulation, it changes the grain to a highly-conductive grain, and, thereby, permits measuring the continuity of the propellant grain by means of electrical conductance measurements. These conductance measurements provide means of assessing the changes which take place in the solid propellant grain, such as, the physical and chemical changes (which affect mechanical properties) which the grain has undergone during storage or aging or when the grain is subjected to different load conditions, such as, acceleration, blast, shock, etc. In addition to the benefit of the reliable means for assessing such changes, the propellant grains employing the tungstates show an unpredicted increase in the propellant burning rate. The propellant density also increased due to the high density of the tungsten bronzes, and this is another benefit.read more
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Patent
Solid propellant service life analysis via nondestructive testing
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Patent
Method for electrically initiating and controlling the burning of a propellant charge and propellant charge
Henrik Almstrom,Bjarnholt Gert +1 more
TL;DR: In this article, a propellant charge consisting of a compact propellant and a method for electrically initiating and controlling the burning of such a charge is described, where electrothermal energy is supplied to the charge by feeding electric current over electrically conductive surfaces (6, 7, 19) in the propellant.
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Heat shielding material and method for manufacturing the same
TL;DR: In this paper, a heat shielding material and a method for manufacturing thereof is provided. But, the method of manufacturing the material, which includes: providing a tungsten oxide precursor solution containing a group VIII B metal element, drying the tungstens oxide precursor to form a dried tungstein oxide precursor; and subjecting the dried Tungstenstein Oxide precursor to a reducing gas at a temperature of 100° C to 500° C.
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Patent
Igniter charge for propellant compositions and rocket propellant charges
TL;DR: The present disclosure as mentioned in this paper relates to an IGNITER CHARGE for PROPELLANT POWDER CHARGES and ROCKET PROPPELLANT CHARGES COMPRISING A HOT PARTICLEIGNITER MASS CONTAINING A BINDER SELECTED from the Group Consisting of POLYEPOXIDES, POLYESTERS,POLYURETHANES, POLyBUTANDIENES, PolYOLEFINS, SILICONES, CELLULOSE DERIVATIVES, AND RUBBER, and OXY
Patent
Liquid polynuclear hydrocarbyl ferrocenes
Thomas P Rudy,Harry J Hyer +1 more
TL;DR: In this article, a mixture of polynuclear hydrocarbyl substituted ferrocene compounds, each of which is substituted with at least one hydrocar-byl group, the total number of carbon atoms in the substituents of each substituted Ferrocene nucleus being in the range of from 1-6, said compositions being noncrystalline, non-crystallizable liquids having an average molecular weight no greater than about 950, and being combustion catalysts for composite solid propellants.
Patent
Method of curing propellants containing carboxyl terminated polyalkadienes using an organic iron salt
Grant Thompson,Bobby M Wall +1 more
TL;DR: In this article, a method of producing superior cures in SOLID PROPELLANT COMPOSITIONS is described. But this method is not suitable for the case of cancer patients.
Patent
Combination burning rate catalyst and curative
TL;DR: Epoxyethylferrocene was used as a combination burning rate catalyst and curative in a solid propellant composition as discussed by the authors, but it was not considered curative enough to be used in a firework.
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