liquid rocket的例句大全

Based on a space liquid rocket engine system, the static and dynamic characteristic of pressure-fed Liquid Propellant Rocket Engine was studied, furthermore, analyses of the static and dynamic characteristic were also carried out for the valve of the system.

本文以挤压式液体火箭发动机为研究对象，以工程研制为背景，对小型的空间液体火箭发动机系统进行静态特性及动态特性的研究，并且对系统中的电磁阀的静、动态特性进行了分析。

The Study and Development of Skin Protective Equipment for Liquid Rocket Propellant

火箭推进剂皮肤防护装备研究现状及发展趋势

As the carrier of spaceflight and martial arms, the propellant in liquid rocket should be measured.

液体火箭作为载人航天技术和军事武器的载体, 通常需要对其推进剂储箱中的燃料进行液位测量.

POGO vibration is a low-frequency vibration problem which can not be ignored in the course of liquid rocket flight, it belongs to fluid-solid coupling dynamics.

POGO振动是大型液体火箭飞行过程中遇到的一个不容忽视的低频振动问题，属于流固耦合动力学研究范畴。

Fuzzy min-max neural networks and its application to liquid rocket engine failure classification

模糊极小极大神经网络在火箭发动机故障分类中的应用

Considering the typical application background of the LH2/ LOX rocket engine turbopump, this paper discusses the development of the investigation about the hybrid bearing for the liquid rocket engine turbopump.

以液体火箭发动机涡轮泵为典型应用背景，讨论了液体动静压滑动轴承的技术特点及其用于液体火箭发动机涡轮泵转子支撑的研究进展情况；

Application of Electrochemical Gas Sensor on Detection of Liquid Rocket Propellant

控制电位电解型气体传感器在液体推进剂检测中的应用

Disigning coolant channel on the firebox of liquid rocket engine to loxodrome ( equal-angle helix) groove can improve firebox coolant capability greatly.

将液体火箭发动机燃烧室的冷却通道设计为斜航线（等倾角螺旋线）槽形，可以大幅度改善燃烧室的冷却性能。

The leak of Liquid Rocket Engine ( LRE ) is very common and dangerous.

液体火箭发动机的泄漏是常见和极其危险的故障.

The major failure models of liquid rocket engines of foreign countries and china are analyzed.

分析了国内外液体火箭发动机主要故障模式；

As one of the few advanced countries in liquid propulsion, France actually began to study and develop liquid rocket engine on the morrow of World War II.

法国是开展液体推进技术研究较早的国家之一，也是当前世界上液体推进技术比较先进的一个国家，但他们在这一领域也经历了一个漫长曲折的发展过程。

The two phase turbulent combustion steady process and high combustion instability in the liquid rocket engine are simulated with the method of computational combustion dynamics.

采用计算燃烧学的方法对发动机燃烧室内的湍流两相燃烧过程的稳定燃烧状态和高频不稳定燃烧现象进行了数值模拟。

A new modular method is proposed for static simulation of liquid rocket engine.

提出了一种新的液体火箭发动机静态仿真模块化计算方法.

To review the progress in the major assignment, the organization and implementation of protection against liquid rocket propellent.

综述了发射大型运载火箭推进剂作业卫勤保障主要任务、保障重点、卫勤力量的分配、卫勤保障的组织和实施进展。

Fault diagnosis of liquid rocket engine based on immune Agent

基于免疫Agent的液体火箭发动机故障诊断

The complex flow was simulated with sequential and parallel SIMPLE algorithm in the combustion chamber of liquid rocket engine.

用串行和并行SIMPLE算法对液体火箭发动机燃烧室内的复杂流动进行了数值模拟。

Environmental factor of Weibull distribution for liquid rocket engine failure

液体火箭发动机失效的Weibull分布环境因子

The article hereunder describes the history of liquid rocket propulsion in France through the last 50 years.

本文回顾了法国液体火箭推进技术在过去50年间的发展历史。

Application of Elman Neural Network on Liquid Rocket Engine Fault Prediction

Elman型神经网络在液体火箭发动机故障预测中的应用

A Real-time Fault Diagnosis Approach to Liquid Rocket Propulsion Systems Using Mechanism Model and SOM Neural Networks

一种应用机理模型和SOM神经网络的液体火箭推进系统实时故障诊断方法