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1·By 2010 Brown and other astronomers had discovered 15 more of these hypervelocity stars.

2010年，布朗和其他天文学家又发现了15颗这样极高速运行的恒星。

2·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。

3·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。

4·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。

5·We can get electron density with the calculated phase and some common model formula in the wake of hypervelocity projectiles.

由计算出的相位并根据弹道靶尾迹的一些常用模型公式，把相位转化为尾迹的电子密度。

6·The oblique detonation stabilized on a hypervelocity projectile was researched by numerical simulations and experimental visualizations.

通过数值模拟和实验显示的方法对驻定在高速飞行体上斜爆轰波流场进行研究。

7·A new design method for establishing the thrust scheme and overall performance parameters of hypervelocity kinetic antitank missile is provided.

目的在于为确定高速动能弹的推力方案和总体参数提供一种新的设计方法。

8·The results of theoretical analysis, numerical simulation and experiments show that the hypervelocity flyers can be obtained by this technology.

理论分析、数值模拟和实验结果表明，由这种方法获得超高速飞片是可行的。

9·The phenomenon of aerodynamic heating and ablation for hypervelocity projectues seriously affects the characteristics of the exterior ballistics.

超高速弹箭存在的气动加热烧蚀现象会严重影响其外弹道特性。

10·Both the damage effectives of hypervelocity impact on spacecraft and the thin plate shield method for hypervelocity impact resisting are outlined.

概述了超高速碰撞对空间飞行器的破坏效应，简述了防护超高速碰撞的薄板屏蔽方法。

超高速

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。