liquid propellant

liquid propellant

美 　英

• un.液体燃料；液体推进剂；液体火箭燃料
• 网络液态推进剂；液体推动药；液体发射药

英汉解释

un.	1. 液体燃料 2. 液体推进剂 3. 液体火箭燃料

例句

The application of a pressure difference across an injector does not cause an immediate velocity response of the liquid propellant.

经过喷注器的压降发生变化时并不马上引起液体推进剂速度变化。

This paper introduces theoretical formulation optimization and ignition and combustion experiments of liquid propellant.

文内简述了液体药理论配方优选和液体药点火、燃烧实验研究。

for liquid propellant rocket engine , it is an important condition for effective combustion that propellant be evaporated and mixed quickly.

在液体火箭发动机中，推进剂组元迅速而高效的气化和混和是产生高质量燃烧所必须的重要条件。

It is an important and basic issue to choose monitoring parameters of Liquid propellant Rocket Engine(LRE) monitoring system in ground test.

确定监测参数是液体火箭发动机地面试验监控系统的一个重要而基础的问题。

The characteristics of NIR in liquid propellant are summarized and particular advantages of NIR in liquid propellant are pointed out.

总结了这种分析方法在液体推进剂中的应用特点。

Hydroxylammonium nitrate(HAN) is the main active toxic component of the new HAN based liquid propellant.

硝酸羟胺（HAN）是新型硝酸羟胺基液体推进剂的主要毒理活性成分。

Acceptance testing equipment for production of liquid propellant.

生产液体推进剂用的验收试验设备。

Based on the properties of combustion of droplets of a HAN-based liquid propellant LP1846, a simplified subarea model is presented.

针对HAN基液体发射药LP1846液滴的燃烧特点，建立相应的分区简化模型。

The missile is a single-stage, liquid-propellant design carrying a single nuclear warhead.

导弹是单级，液体推进设计能携带一枚单一的核弹头。

Well and layer selection criteria of liquid propellant high energy gas fracturing (HEGF) are included in this paper.

提出了液体药高能气体压裂选井、选层的条件。

In 1946 S. P. Korolev was charged with heading the development work on ballistic liquid-propellant long-range missiles.

1946年，谢·帕·科罗廖夫担负了领导开发液体推进剂远程弹道导弹的任务。

Study of Regenerative Liquid Propellant Auxiliary Chamber Launching Technique

再生式液体发射药辅助药室发射技术研究

Investigation of a general module simulation method for liquid propellant rocket engines

液体火箭发动机一种通用模块化仿真方法

The Design and Implementation of a Variable Thrust Liquid Propellant Rocket Engine Control System

一种大范围变推力液体火箭发动机控制器的设计及实现

Analysis of Combustion Characteristics for Liquid Propellant Electrothermal Chemical Launcher

液体工质电热化学发射过程燃烧特性分析

Study of Leakage-proof Technique for Storage and Transportation Tanks of Liquid Propellant

液体推进剂贮运设备堵漏技术研究

Finite Element Analysis of the Turbine Blade Structural Characteristics for Liquid Propellant Rocket Engine

液体火箭发动机涡轮叶片结构特性的有限元分析

Flow Analysis and Orifice Plate Design for Oxygen Chamber of a Liquid Propellant Rocket Engine

液体火箭发动机氧腔流动分析及均流板设计研究

Calculation of Bookbinding Parameters and Integrating Method of the Software of Liquid Propellant Utilizing System

推进剂利用系统装订参数计算及软件集成方法

Intelligent damage-mitigating and life-extending control techniques for reusable liquid-propellant rocket engines

液体火箭发动机智能减损与延寿控制技术

Design of a Liquid Propellant Feeding System for Laser Propulsion Thruster

激光推力器液体工质注入系统设计

Modularization modeling and simulation for the transients of liquid propellant rocket engines

液体火箭发动机系统瞬变过程模块化建模与仿真

Method for calculation model establishment in liquid propellant rocket engine numerical simulation

液体火箭发动机数值模拟的计算模型建立方法

Modeling and simulations of the failure process for liquid propellant rocket propulsion systems

液体火箭推进系统故障过程建模与仿真研究

Technologies and methods of the individual decontamination of liquid propellant

沾染液体火箭推进剂时的个人洗消技术进展

Application of evolutionary strategy of research of static characteristics of liquid propellant rocket engine

进化策略在火箭发动机静态特性研究中的应用

Stochastic simulation method of performance reliability estimation on liquid propellant rocket engine

液体火箭发动机性能可靠性的随机仿真方法

first , several models needed in configuration analysis of liquid propellant space propulsion systems are presented in this paper

本文首先建立了在液体推进剂空间推进系统构型分析中所要用到的几种模型。

Study of Atomization in Regenerative Liquid Propellant Gun

再生式液体发射药火炮的雾化问题研究

Independent Component Analysis for Fault Detection of the Liquid Propellant Rocket Engine

独立分量分析在液体火箭发动机故障检测中的应用

Fault diagnosis reasoning for liquid-propellant rocket engines with integration of time information

集成时间信息的液体火箭发动机故障诊断推理

Pressure High-frequency Oscillation in Combustion Chamber of Regenerative Liquid Propellant Gun

再生式液体发射药火炮燃烧室压力高频振荡研究

Application of Support Vector Machine in Steady State Fault Detection and Diagnosis of Liquid-propellant Rocket Engine

支持向量机在液体火箭发动机稳态段故障检测和诊断中的应用

Independent component analysis for the fault features of liquid propellant rocket engine

应用独立分量分析提取液体火箭发动机的故障特征

Bayesian Assessment Method for Performance Parameters of Liquid Propellant Rocket Engine

液体火箭发动机性能参数的贝叶斯评估方法

Design and realization of primitive real-time fault detection and alarm system for liquid propellant rocket engines

液体火箭发动机实时故障检测与报警原型系统的设计与实现

Liquid Propellant Management for the HyperSoar Mobile Vehicle in the Atmospheric Layer

大气层内高超声速机动飞行器液体推进剂管理

Common Accident Treatment in Liquid Propellant Transportation

液体推进剂运输中常见事故的处理

Determination of oxidative damage parameters in mice inhaling mixed liquid propellant

混合推进剂致小鼠氧化损伤指标的测定

Application of Fuzzy Pattern Recognition to Fault Diagnosis of Liquid Propellant Rocket Engines

模糊模式识别技术在液体推进剂火箭发动机故障诊断中的应用