solid rocket的例句大全

In addition, while EKV intercepting of the latter end, the attitude control thrust is provided by the solid rocket motors. When designing the posture control systems, one should fully consider the impact brought by this thrust.

另外，EKV在末段拦截过程中，其姿控推力是由脉冲固体火箭发动机组提供，在设计姿态控制系统时，应充分考虑这种推力形式带来的影响。

It's verified that a series of intense pressure impulses can occur in the combustion chamber after the thrust reversal nozzles of the solid rocket motor are suddenly opened.

实验表明，突然打开固体火箭发动机反向喷管后，燃烧室中可能出现强烈的压力冲击，这种压力冲击来自喷管喉部节流和形成准稳态流动之前的非定常过程。

Technique of thrust termination with reversal nozzle for solid rocket motors

固体火箭发动机反向喷管推力终止技术

Evaluation research of infrared radiation characteristics of solid rocket motor exhaust plume

固体火箭发动机尾焰红外辐射特性预估研究用水龙头把水射向火焰

The experiments indicate that the method making the solid rocket motor as plasma ionizer is effective, and the required electron density value can be gained.

试验表明，将固体火箭发动机作为等离子体发生器是一种行之有效的方法，可以获得需要的电子密度值。

Considering the characteristic that the target is far from the firing point, the operational mission of the long-range air-defense missile and main technical the implementation approach are discussed, namely the optimized trajectory incorporating double-pulse solid rocket motor with double high parabolic trajectory are presented.

针对远程防空导弹拦截的目标远离发射点的特点，讨论了远程防空导弹作战使命及主要技术途径的实现方案，即双脉冲固体火箭发动机和双高抛弹道结合的优化弹道。

The Aerodynamic Design Research of Gas Vane of Solid Rocket

固体火箭燃气舵气动设计研究

Based on the investigation of thrust measurement technique for a rocket engine, a improved method for solving the thrust measurement in the test of the solid rocket engine with single-chamber and. dual-thrust was presented in the paper.

本文通过对某单室双推力发动机推力测试技术的探讨，提出了解决单室双推力固体火箭发动机推力测试技术的改进方法。

Based on the foreign jointing technique between the advanced filament-wound chamber and nozzle, the paper analyzes the jointing modes between chamber and nozzle of an all-composite solid rocket motor and technical approaches, and puts forward the relevant design parameters to give a refrence to designers.

结合国外先进固体发动机纤维缠绕壳体与喷管连接的技术，分析了实现全复合材料固体发动机壳体-喷管的连接方式，技术途径，并提出了有关设计参数，可供设计人员参考。

According to the internal ballistic foreshowing models of solid rocket motors, the interior ballistic performances were simulated and computed by using Monte-Carlo method.

根据固体发动机内弹道性能预示模型，采用Monte Carlo法进行内弹道性能的模拟计算。

Dynamic calculation on thrust vector control system for solid rocket motor

固体火箭发动机推力向量控制系统动力学计算

Two-dimensional axisymmetric transient thermal analysis for a composite construction nozzle of solid rocket motor is performed by finite element method in this paper.

以固体火箭发动机复合结构喷管为对象，用有限元法进行了二维轴对称瞬态热分析。

Four nozzles, canted outboard, split the exhaust of the solid rocket motor into four equal tails.

四个向外倾斜的喷管把固体火箭发动机的排气流分成四个相等的尾巴。

The main contents and conclusions in the paper including: Estiablished the steady numerical models of pintle controlled solid rocket motor, And verified the model with the theoretical experiment data.

建立了喉栓发动机稳态流场的数值模型，用原理试验结果对数值模型进行了校验。

Pegasus is the first air launched solid rocket in America, which is used to place small satellites into low earth orbit.

飞马座火箭是美国第1种机载空中发射型固体运载火箭，主要用于将小型卫星送入近地轨道。

Influence of air mass flow rate ratio on combustion efficiency of solid rocket ramjet with two air inlets

二次进气流量比对固冲发动机燃烧效率的影响

Double mode detection with focused probe was used to inspect the bonding quality in multilayer structure of the solid rocket motor carried by airplane. The method can enhance the test signal energy to obtain effective signal.

针对机载固体火箭发动机多层粘接结构的粘接质量检测问题，利用聚焦探头双模式检测方法提高了检测信号能量，获得有效检测信号。

Did one of the solid rocket boosters somehow burn through its casing?

是否是其中一个助推火箭的外壳因某种原因被烧穿？

Solid rocket motor ( SRM) is an important propulsive component of solid missile and astronautical system. Its dynamic analysis plays a very important role in system stability and vibration environment forecast.

固体火箭发动机是固体导弹和宇航系统的重要元件，它的动力学分析对系统稳定性、振动环境预测有重要的意义。

Research on internal ballistics calculation uncertainty of solid rocket motors

固体发动机内弹道计算不确定性研究