Acceptance testing equipment for production of liquid propellant.
生产液体推进剂用的验收试验设备。
Theoretically, any liquid propellant may be manufactured into gelled propellant.
从理论上说，任何液体推进剂都可以制成胶体推进剂。
Some stratification exists in the spray produced by any liquid propellant injector.
由任何液体推进剂喷注器所产生的喷雾都存在某些成层现象。
The tests include the leak detection of liquid propellant and other liquid systems.
完整性试验包括对推进剂和其它液体系统的泄漏检测。
The membrane tank is that one kind of liquid propellant of space system is broad used.
隔膜贮箱是一种空间系统应用较广泛的液体推进剂贮箱。
The modeling of priming process of Liquid Propellant Rocket Engines (LPRE) was studied.
研究了常温推进剂液体火箭发动机充填过程的建模问题。
Flow in injector passages of a variable thrust liquid propellant rocket engine was studied.
本文对变推力液体火箭发动机喷注器通道内介质流动进行求解。
Propellant feeding system is indispensable to laser propulsion thruster with liquid propellant.
工质注入系统是液体推进剂激光推力器必不可少的一个组成部分。
Some Suggestions and proposals for the future application of nano-technology in liquid propellant...
提出了今后在液体火箭发动机中采用纳米技术的设想和建议。
Liquid propellant combustion processes are quite complicated and defy precise analytical description.
液体推进剂燃烧过程是相当复杂的，很难对其进行严谨的分析描述。
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。
CZ-2C is a two-stage liquid propellant launch vehicle, which is suitable for launching heavier LEO satellite.
CZ - 2c是适用于发射低轨道、质量较大卫星的二级液体运载火箭。
Objective To establish model of the blast-toxicosis combined injury caused by the explosion of the liquid propellant.
目的复制冲击波和液体火箭推进剂中毒致冲毒复合伤的动物模型。
A neural network classifier that utilizes fuzzy sets as failure classes of a liquid propellant rocket engine is studied.
研究了一种用模糊集表示火箭发动机故障模式的神经网络分类器。
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。
Noise in the raw acquired data of liquid propellant rocket engine test can reduce accuracy and creditability of the data.
液体火箭发动机试验的原始测量数据中存在着噪声，影响了数据的准确性和可信性。
Several key problems existed in field operation of liquid propellant are solved and field experiment results are given also.
解决了液体药现场施工过程中的几个关键问题，并给出了现场试验效果。
Its can be applied to evaluate the harmfulness of the liquid propellant rocket explosions for the space vehicle launching site.
理论和实验研究结果可用于航天发射场发生液体火箭爆炸的危害性评估。
A theoretical model has been presented to describe the combustion process in a liquid propellant electrothermal chemical launcher.
该文提出描述液体工质电热化学发射装置中燃烧过程的理论模型。
The general integral equations are derived for liquid and gas components of space propulsion systems with liquid propellant rocket engine.
针对采用液体推进剂火箭发动机的空间推进系统，推导了系统液路和气路的通用积分形式方程。
Also, a formula calculating the pressure drop of series throttle holes in the liquid propellant transporting system is given in this paper.
文中还给出了液路系统中各串联节流孔压降公式。
To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood.
为了分析液体推进剂火箭发动机燃烧室中存在的非稳态环境，必须很好地了解稳态状态。
The structure design for sloshing suppression in a liquid propellant tank results in the nonlinear characteristics of liquid sloshing damping.
液体推进剂贮箱的防晃结构设计导致液体晃动阻尼的非线性特性。
The dynamic models of engine parts in a new high-performance staged combustion cycle liquid propellant rocket through the module codified were built.
通过模块化编程，建立了新一代高性能补燃发动机启动过程的部件模型。
There is no evidence that the overdose of free radicals is produced and lipid peroxidation occurs when the animals are exposed to high dose of liquid propellant.
高浓度的混合推进剂中毒时，自由基产生相对减少，机体外周血和肺外器官不发生显著的脂质过氧化损伤。
This paper attempts to analyse the tendency to develop liquid propellant rocket propulsion technology according to the requirements o launch vehicles and spacecrafts.
本文试图根据运载火箭和航天器的需要来分析液体火箭推进技术的发展趋势。
Positive pressure light protective appliance for liquid propellant was manufactured, by using the electric airing technology, the dressed comfortability was enhanced.
研制了一种能有效防护液体火箭推进剂的正压式轻型防护服，利用电动送风技术，极大提高了穿着的舒适性。
This paper presents the development of the liquid propellant rocket engine technology from the viewpoint of combustion chamber pressure, thrust level and power cycle.
本文从燃烧室压力、系统工作循环方式以及最大推力三个方面叙述了世界各国液体火箭发动机的技术水平。
This paper relates to the current development, fire mechanism, operating mode and development tendency of liquid propellant gun and presents its features and advantages.
本文简述了舰载液体发射药火炮研制概况、发射机理、工作方式、目前研制方向和重点，分析了液体发射药火炮的特性和优点。
This paper relates to the current development, fire mechanism, operating mode and development tendency of liquid propellant gun and presents its features and advantages.
本文简述了舰载液体发射药火炮研制概况、发射机理、工作方式、目前研制方向和重点，分析了液体发射药火炮的特性和优点。
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