1·The results of spacecraft space debris shield configuration, as well as pressure vessel damage behavior characteristic under hypervelocity impact conditions are presented as applications.
作为应用的例子给出了超高速撞击条件下航天器空间碎片防护结构以及压力容器损伤特性实验研究的结果。
2·The range equipment for the investigation of the hypervelocity aerodynamic properties and flow field of explosively formed projectile(EFP) models is described.
本文描述的是研究爆炸成型发射弹（EFP）模型的流场及超高速空气动力特性所用的弹道试验设备；
3·A numeral model of erosion for carbon-based materials impacted by hypervelocity particles was established based on dynamics.
应用动力学理论建立了碳基材料超高速粒子侵蚀的数学模型。
4·Skin of spacecraft is usually considered as the most basic shield structure against hypervelocity impact of space debris.
航天器的蒙皮是抵御空间碎片超高速撞击的最基本防护结构。
5·Investigates the distribution characteristics of secondary debris clouds generated during a hypervelocity oblique impact.
研究超高速斜碰撞所形成的二次碎片云的分布特性。