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本文系由AD267480报告编译写成。它介绍了由美国飞机武器装备公司,在60年代初期为“中士”导弹头部研制和发展的一种强力径向抛射战斗部。该战斗部重量为732kg,装有E130R2型球形子弹,363kg。战斗部在目标上空约3000米的高度上打开母弹壳体,抛射装置将子弹沿径向抛射开来,使子弹均匀的散落在半径为600米的范围内。该战斗部约经历了两年左右的研究和试验,取得了成功。本文着重介绍了这种强力径向抛射装置的作用原理、结构设计、径向抛射理论以及静态点火试验、飞行试验的结果和分析。虽然,目前这种类型的强力径向抛射装置已逐步被更加先进的离心式抛射装置所代替,如“长矛”导弹T-22的M251型球形杀伤子母弹战斗部,就进行了这种替换,但它在研制中所遇到的种种问题和经验,仍可作为我们有益的借鉴。
This article written by the AD267480 report compiled. It introduced a powerful radial projectile warhead developed and developed by the U.S. aircraft and weaponry company for the “Sergeant” missile head in the early 1960s. The warhead weighs 732kg, equipped with E130R2 spherical bullets, 363kg. The warhead opens the projectile shell at a height of about 3,000 meters above the target and the projectile throws the projectile in a radial direction so that the bullets scatter evenly over a radius of 600 meters. The warhead has experienced about two years of research and experimentation and achieved success. This article focuses on the principle of this powerful radial projectile device, structural design, radial projection theory and static ignition test, flight test results and analysis. Although this type of powerful radial projectile has now been gradually replaced by more advanced centrifugal projectiles, such as the M251 ballistic warhead warhead of the Spear missile T-22, However, all the problems and experiences it encounters in the course of research and development can still serve as our useful reference.