高压物理学报2011，Vol.25Issue(6)：557-564,8.
一种基于二级轻气炮平台的超高速弹丸发射装置设计
A Novel Design of a Hypervelocity Launcher Based on Two-Stage Gas Gun Facilities
摘要
Abstract
A new scheme of hypervelocity launcher was put forward in this paper by means of strong detonation. An explosive ring was fixed internally in a specially designed third-stage barrel in which the projectile launched by two-stage gas gun at velocity ranging from 6 to 7 km/s was able to be accelerated subsequently to a hypervelocity of 10 km/s or so. Based on hydrocode simulations, the shape of flyer and explosive ring was optimally designed. In addition, through the encapsulation of the sphere projectile by epoxy resin, the projectile damages resulted both from detonation-induced jet and spalling due to the characteristic of short pressure pulse imposed on centimeter-sized projectiles would he suppressed. The simulations illustrate that the optimized hypervelocity launcher has the capability of accelerating 1.03 g aluminum alloy projectile with a velocity of 6 km/s to 9.6 km/s, keeping the sphere-like shape withthe velocity amplification ratio of 1.6.关键词
超高速发射装置/强爆轰/流体动力学模拟/AUTODYNKey words
hypervelocity launcher/strong detonation/hydrocode simulations/AUTODYN分类
数理科学引用本文复制引用
赵士操,宋振飞,姬广富,龚自正,赵晓平..一种基于二级轻气炮平台的超高速弹丸发射装置设计[J].高压物理学报,2011,25(6):557-564,8.基金项目
国防科技重点实验室基金 （）
国防科工局空间碎片项目 （）
