首页> 外国专利> COMBINED CHARGE OF SOLID PROPELLANT ROCKET ENGINE WITH FLAME ARRESTING EFFECT OF EFFLUENT JET OF COMBUSTION PRODUCTS (VERSIONS)

COMBINED CHARGE OF SOLID PROPELLANT ROCKET ENGINE WITH FLAME ARRESTING EFFECT OF EFFLUENT JET OF COMBUSTION PRODUCTS (VERSIONS)

机译:固体推进剂火箭发动机的混合装料与燃烧产物(版本)的射流火焰阻滞作用

摘要

FIELD: engines and pumps.;SUBSTANCE: combined charge of solid propellant rocket engine with flame arresting effect of effluent jet of combustion products includes solid-propellant grain and grain of flame arresting compound, which is installed near one of edges of solid-propellant grain. As per the other version, charge of solid propellant rocket engine is made in the form of multi-grain charge including several grains of flame arresting compound, which are equally located along the perimetre. In each of the versions the fire arch of grain of flame arresting compound and its weight are made considering the ratios determined by this invention.;EFFECT: invention allows improving reliability and safety of solid propellant rocket engine.;6 cl, 2 dwg
机译:领域:发动机和泵;物质:固体推进剂火箭发动机的组合装料与燃烧产物废气喷射的阻火作用包括固体推进剂颗粒和阻火化合物颗粒,安装在固体推进剂颗粒边缘之一附近。与其他版本一样,固体推进剂火箭发动机的装药是以多颗粒装药的形式制成的,包括几粒阻火化合物颗粒,这些颗粒沿炮弹等距分布。在每种形式中,考虑到本发明确定的比例来制成阻火化合物颗粒的火弓及其重量。效果:本发明可以提高固体推进剂火箭发动机的可靠性和安全性; 6 cl,2 dwg

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