首页> 外国专利> Propellant charge for shell projectiles or rockets has a core charge with a firing system and a surrounding compact charge with a separate time-delayed firing system to fire it in fractions with the core to accelerate the developed gas vol

Propellant charge for shell projectiles or rockets has a core charge with a firing system and a surrounding compact charge with a separate time-delayed firing system to fire it in fractions with the core to accelerate the developed gas vol

机译:用于弹丸或火箭的推进剂装药具有带有发射系统的堆芯装药和带有单独的延时发射系统的周围紧凑装药,可与堆芯一起进行分段燃烧,以加速所产生的气体体积

摘要

The propellant charge (1), for a shell projectile or rocket, has a conventional core charge with a firing system (4). The core is contained within a compact charge (3) shrouding, with its own firing system (5) of electrical conductors (6,7) with a high electrical energy, with a controlled time delay after firing the core charge. During the combustion of the core charge, the surrounding compact charge is fired in fractions with a regular geometry. The fractions accelerate the gas vol. developed by the combustion of the core charge.
机译:对于弹丸或火箭,推进剂装药(1)具有常规的带有射击系统(4)的装药芯。芯包含在紧凑的装药(3)罩中,其自身的点火系统(5)具有高电能的电导体(6,7),在发射芯装药后具有受控的时间延迟。在堆芯装药燃烧期间,周围的紧密装药以规则的几何形状分批燃烧。这些馏分加速了气体体积。由核心装药的燃烧产生。

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