这种冲击波被称为直线弹道式体外冲击波。
This shock wave is called rectilinear ballistic extrinsic shock wave.
本文提出了弹道式飞行器自由飞行轨道的解析解法。
In this paper an analytic solution of free flight trajectory of ballistic vehicle is presented.
我认为我们不会进行(弹道式着陆)，但假若进行，我也不会担心。
I don't think we are going to have one (ballistic landing), but if we did, it would not concern me.
去年，搭载马拉西亚首位宇航员的“联盟号”返回舱也因螺栓问题来了个“弹道式”着陆。
Last year, a Soyuz capsule carrying Malaysia's first astronaut also made a so-called "ballistic" landing, similarly blamed on faulty bolts.
由于考虑了加速度的实时估计，该滤波方法尤其适用于对弹道式目标的机动跟踪。
Because of the taking into consideration of the real time acceleration estimation, this filter method is applicable to maneuverable tracking of the target using its trajectory data.
级间热分离具有改善和提高继续飞行级的稳定性和入轨精度而被固体弹道式导弹广泛采用。
The thermal stage separation being provided with improving and enhancing stability and orbit precision for flight was abroad adopted in solid-propellant ballistic missile.
去年，搭载马拉西亚首位宇航员的“联盟号”返回舱也因螺栓问题来了个“弹道式”着陆。
Last year, a Soyuz capsule carrying Malaysia "s first astronaut also made a so-called" ballistic "landing, similarly blamed on faulty bolts."
介绍弹道式再入航天器烧蚀防热结构设计，文中说明了方案、材料选择、设计和分析计算。
This paper introduces ablative thermal protection structure design of a return module of some satellites.
对某型二级弹道式导弹进行了最大射程弹道优化，并将得到的最大射程弹道与原弹道进行了比较分析。
As an example, maximum trajectory optimization was applied on a two-stage ballistic missile, and a comparison of original and optimal trajectories was presented with figures and tables.
以等高程和等过载引信两种弹头引信方式建立了大气参数偏差对弹道式导弹弹头引爆点射程影响的数学模型；
A mathematical model is established solely according to two kinds of warhead fuze modes considering that atmosphere parameter error works on the flight of warhead explosion spot of ballistic missile.
弹道式飞行器再入时，常常要求在规定高度上发出开伞信号，过载延时控制方法误差太大，不能满足精度要求。
The opening parachute signal is required to sent on the fixed height when the vehicle reentry. The height controlled error through axis apparent acceleration can not meet the required precision.
这些新功能将建立在一个开放式系统架构，以便将任何传感器和武器系统纳入弹道导弹防御系统(BMDS)。
These new capabilities will be built upon an open systems infrastructure to facilitate the ability to incorporate any sensor and weapon system into the Ballistic Missile Defense system (BMDS).
由于再生式液体发射药火炮的结构复杂，故数值模拟对研究内弹道参数对系统的影响具有重要作用。
Due to the complex structure of RLPG, numerical simulation is of great importance for studying the influence of interior ballistic parameters on the system performance.
根据复杂的分装式混合装药的特点，建立起多相流内弹道模型。
In this paper, two-phase flow interior ballistic model is set up on the basis of the characteristics of complicated separate loading mixed charges.
用固体火箭发动机中常用的瞬态平衡压强法对烟火剂式点火器内弹道性能进行了理论预示，并提出热损失系数的概念。
Instantaneous equilibrium pressure method is used in this paper to analysis the internal ballistics of pyrogen-type igniters. A concept of igniter heat loss coefficient is also presented.
靶场实验结果表明，利用该方法所测出的火箭助飞式声干扰器的空中弹道特性对其研制过程有一定指导意义。
The results of the range experiment indicate that the air ballistic characteristic tested by this method is directive to the research and development of a rocket-propelled acoustic jamming equipment.
再生式液体发射药火炮在内弹道循环中，膛内除弹丸运动外，还存在活塞压缩液体燃料的运动。
In the interior ballistic cycle of regenerative liquid propellant gun, in addition to motion of projectile, there exists motion of piston compressing the liquid propellant.
本文针对小型子母式催泪弹，采用经典弹道理论建立了高低压室发射方式的内外弹道数学模型。
Based on conventional ballistics theory, the mathematical model of the ballistic trajectory which adopts low and high pressure chamber fire mode is established for the small cluster tear bomb.
针对再生式液体发射药火炮(RLPG)内弹道过程中非稳态喷雾燃烧流动问题，建立了数学模型，给出了具体的计算方法。
Aimed at nonsteady spray combustion flow problems of regenerative liquid propellant gun (RLPG) in process of interior ballistic, mathematical model was established, and numerical method was derived.
为满足弹道散布范围大或大口径弹丸的测速场合，提出了一种原向反射式激光光幕测速的方法。
A novel laser screen method with retroreflector for velocity measurement is introduced for some special velocity measuring occasions like wide spreading range or large caliber projectiles.
用增阻系数的概念，建立了增阻式射程弹道修正弹的质心运动方程组。
The mass center motion equations of a damp-increasing range correction projectile were established by the concept of damp-increasing coefficients.
研究了助推-滑翔式弹道中段的近似解。
The approximate solutions of the mid-course trajectories for the boost-glide vehicles are investigated.
推导出了计算低速低伸外弹道的解析式。
The analysis solution of outer trajectory about low speed and flat trajectory is deduced out.
分析燃气蒸气式发射动力系统内弹道计算产生误差的影响因素。
This paper analyzed the influencing factors of errors of interior ballistic calculation in gas and steam type launch power system.
用增阻系数的概念，建立了增阻式射程弹道修正弹的质心运动方程组。
The mass center motion equations of a damp-increasing range correction projectile were …
用增阻系数的概念，建立了增阻式射程弹道修正弹的质心运动方程组。
The mass center motion equations of a damp-increasing range correction projectile were …
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