液体推进剂

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。

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

有机结合PVT和BK法以降低测量卫星液体推进剂的不确定度

Reduction of measurement uncertainty of liquid propellant remaining on satellite by combining PVT with BK organically

通过与实验结果进行对比，验证此法可行，能够用来模拟HAN基液体推进剂的高压燃烧过程。

This method is feasible by comparing the simulation results with the experimental data , so it can be used to simulate the high-pressure combustion process of HAN-based liquid propellants .

黏合剂活性基团对HTPB推进剂力学性能的影响机制双组元液体推进剂远地点发动机

Mechanism of influence of active groups in binder on mechanical properties of HTPB propellants bipropellant liquid apogee motor

HAN基液体推进剂是一种新型绿色高能液体推进剂，是液体火箭发动机的理想燃料之一，其燃烧特性的优劣直接影响到发动机的工作性能。

HAN-based liquid propellant is a new type of green high-energy liquid propellant , whose combustion behaviors will directly affect the performance of the engine , as an ideal fuel for the liquid rocket engine .

本文介绍了基于GPIB总线接口和PC计算机的液体推进剂火箭爆炸污染参数测试系统，叙述了该系统的硬件组成和软件方案。

This paper introduced a test system developed for the research on the explosion pollution of liquid propellant rocket . This system is based on the GPIB bus interface and PC computer .

应用统一建模语言和Synergy软件过程模型建立了液体推进剂空间推进系统构型分析软件的软件模型。

Software model of the study of the software of configuration analysis of liquid propellant space propulsion systems is presented in this paper using Unified Modeling Language and Synergy software process model .

偏二甲肼（UDMH）是液体推进剂的主体燃料，其对水体的污染一直倍受重视。

Unsymmetrical dimethylhydrazine ( UDMH ) is the main fuel of liquid rocket propellant . Stress is always laid on the pollution of UDMH to water .

本文介绍了LP-1型液体推进剂自动分析仪控制系统的软件设计原理、软件结构及控制软件的处理流程。

The designation principle , structure and processing flow of software for the control system of the automatic titration instrument were introduced in this paper .

目的观察N-乙酰半胱氨酸（NAC）对大剂量火箭液体推进剂偏二甲基肼（UDMH）和四氧化二氮（N2O4）吸入性急性肺损伤（ALI）的保护性作用。

Objective To investigate the protective effect and its mechanisms of N - acetylcysteine ( NAC ) on acute lung injury ( ALI ) caused by exposure to high concentration rocket liquid propellants asymmetrical dimethylhydrazine ( UDMH ) and dinitrogen tetroxide ( N2O4 ) .

为了分析其故障特性和获取各种动态故障模式，采用性能优良的Runge-Kutta-Fehlberg（R-K-F）方法求解动态故障模型方程，仿真液体推进剂导弹（液体导弹）动力系统全系统动态故障。

In order to analyze dynamic fault characteristic and acquire all dynamic fault patterns , the Runge-Kutta-Fehlberg ( R-K-F ) method is employed to solve equations of dynamic model for the whole missile power system .

高能可贮性液体推进剂（胺肼-10与硝酸-40S）

High-energy storable liquid propellant ( amine hydrazine-10 and nitric acid-40s )

控制电位电解型气体传感器在液体推进剂检测中的应用

Application of Electrochemical Gas Sensor on Detection of Liquid Rocket Propellant

对液体推进剂质量分析方法的发展进行了综述。

The evolution of quality analysis for liquid propellant is reviewed .

利用报废的液体推进剂硝酸-27S和乙醛制备乙二醛。

Glyoxal is prepared with waste liquid propellant HNO3-27S and ethanal .

液体推进剂液滴高压蒸发研究

A Study of Evaporation of Liquid Propellant Droplet under High Pressure

液体推进剂偏二甲肼氧化变质的规律和影响因素

Investigation on Characteristics and Influencing Factors of Oxidation Process of UDMH

液体推进剂之间的迅速反应可能导致混合不良。

Rapid reactions between liquid propellants can lead to inefficient mixing .

自动电位滴定法分析液体推进剂单推三的研究

Study on automatic potentiometric titration in analysis of liquid propellant DT-3

从理论上说，任何液体推进剂都可以制成胶体推进剂。

Theoretically , any liquid propellant may be manufactured into gelled propellant .

航天靶场液体推进剂的泄漏研究与污染控制

Leakage study and pollution control for liquid propellant in space launch set

跨大气层和空间区域飞行器的液体推进剂管理

Research on Liquid Propellant Management for Cross Atmospheric Layer and Space Vehicle

液体推进剂一甲肼与水二元物系汽液相平衡的研究

Studies on vapor liquid equilibrium of Monomethylhydrazine water binary system

液体推进剂液雾序列脉冲电点火特性研究

Study on Properties of Series Pulse Electrical Ignition of Liquid Propellant Spray

液体推进剂空间发动机系统对质心漂移的影响

Effect of liquid propellant space engines system on centroid drift

液体推进剂火灾爆炸事故类型分析及其预防

Analysis of fire and explosion accidents of liquid propellants and the prevention

常规液体推进剂作业安全性研究

The Quantitative Safety Analysis of Conventional Liquid Rocket Propellant Operation

火箭低温液体推进剂增压系统数学模型

The Numerical Model of Rocket Cryogenic Liquid Propellant Pressurization System

液体推进剂中氧化剂废水处理方法研究

Study of method for treating oxidant wastewater of liquid propellant

液体推进剂偏二甲肼自动电位滴定分析方法的建立

The Establishment of the Automatic Potentiometry for Unsymmetrical Dimethylhydrazine Analysis