首页> 外国专利> BINDING COMPOSITION FOR IMPREGNATION OF REINFORCING MATERIAL AT ARMOURING OF SOLID PROPELLANT CHARGES BY WINDING METHOD

BINDING COMPOSITION FOR IMPREGNATION OF REINFORCING MATERIAL AT ARMOURING OF SOLID PROPELLANT CHARGES BY WINDING METHOD

机译:缠结法固溶推进剂装甲时浸渍增强材料的粘结剂组合物

摘要

FIELD: rocketry, in particular, binding compositions for impregnation of reinforcing materials (glass fibers, glass belts) at armouring of solid propellant charges by the winding method.;SUBSTANCE: offered is a binding composition containing epoxydianil resin with molecular mass 390-430, expoxydianil resin with molecular mass 480-540, epoxydianil resin, product of condensation of trimethylpropane with epilchlorohydrin, isomethyltetrahydrophtal anhydride. Solidified composition of the binder with a high heat resistance (up to 145 C) is obtained.;EFFECT: enhanced resistance of articles to aerodynamic heating.;2 tbl
机译:技术领域:火箭技术,特别是用于通过缠绕法在固体推进剂装料的铠装中浸渍增强材料(玻璃纤维,玻璃带)的粘合剂组合物;物质:提供一种包含分子量为390-430的环氧二苯胺树脂的粘合剂组合物,分子量为480-540的环氧二苯胺树脂,环氧二苯胺树脂,三甲基丙烷与环氧氯丙烷缩合的产物,异甲基四氢邻苯二甲酸酐。获得了具有高耐热性(最高145 C)的粘合剂的固化组合物。效果:增强了制品对空气动力加热的耐受性; 2 tbl

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