生产液体推进剂用的验收试验设备。
Acceptance testing equipment for production of liquid propellant.
总结了这种分析方法在液体推进剂中的应用特点。
The characteristics of NIR in liquid propellant are summarized and particular advantages of NIR in liquid propellant are pointed out.
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.
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 membrane tank is that one kind of liquid propellant of space system is broad used.
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.
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。
Some stratification exists in the spray produced by any liquid propellant injector.
利用液体火箭发动机作动力装置的火箭，又称液体推进剂火箭。
Steady state fault detection and diagnosis of liquid propellant rocket engines based on decision tree method;
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。
Propellant feeding system is indispensable to laser propulsion thruster with liquid propellant.
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 structure design for sloshing suppression in a liquid propellant tank results in the nonlinear characteristics of liquid sloshing damping.
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。
Liquid propellant combustion processes are quite complicated and defy precise analytical description.
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.
讨论了航天发射场液体推进剂泄漏及蒸汽逸散的模式，并建立了定量分析模型。
The pattern of liquid rocket propellant seep and steam diffusion is discussed in this paper, and the model of quantitative analysis is also established.
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。
To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood.
而印度的极卫星运载火箭（PSLV）只能使用固体和液体推进剂，载荷能力也小于两吨。
The Polar Satellite Launch Vehicle (PSLV) uses only solid and liquid propellants and is capable of carrying payloads less than 2 tonnes.
该方法能快速准确的检测和诊断液体推进剂贮运的潜在故障，对推进剂安全贮运有一定裨益。
This method can quickly and accurately check and diagnose the potential fault of the liquid propellant store and transport, which would be benefit for liquid propellant safe store and transport.
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。
The general integral equations are derived for liquid and gas components of space propulsion systems with liquid propellant rocket engine.
液体推进剂的晃动特性对大型液体运载火箭以及战略弹道导弹的飞行动力稳定性有着很大的影响。
The dynamic behavior of the liquid sloshing has great effect on the dynamic stability of the liquid filled space vehicle and the strategical ballistic missile.
液体推进剂的晃动特性对大型液体运载火箭以及战略弹道导弹的飞行动力稳定性有着很大的影响。
The dynamic behavior of the liquid sloshing has great effect on the dynamic stability of the liquid filled space vehicle and the strategical ballistic missle.
比较全面地介绍了适合我国卫星液体推进剂测量的气体注入压力激励方法，对相关应用技术问题进行了分析讨论。
The method, called pressure stimulation by gas injection, was introduced in detail for the measurement of liquid propellant residue on the national satellite. A technical scheme in practice was given.
对液体推进剂在贮运过程中发生的泄漏情况进行了深入分析，建立了故障树模型，并讨论了底事件对泄漏事件的影响。
This paper analyzes the leakage that may occur during the liquid propellant store and transport, builds up the leakage fault tree and discusses how the basic incident affects the leakage incident.
分析了固液发动机推进剂的燃烧特性和发动机性能特性、与液体和固体火箭发动机的不同，以及研制的技术难度等。
The propellant feature of burning behavior and engine in hybrid engine, the differences to liquid and solid engine and the difficulties of technology in development were analyzed.
第一个使用液氧碳氢推进剂的国产液体燃料火箭发动机被安装在了火箭的E段上，它可以提供5.6吨的推力。
The first native liquid-fueled rocket engine used a liquid oxygen and carbon-hydrogen propellant, provided 5.6 tons of thrust, and was installed in unit e.
研究了常温推进剂液体火箭发动机充填过程的建模问题。
The modeling of priming process of Liquid Propellant Rocket Engines (LPRE) was studied.
结论液体火箭推进剂致伤后的远期效应明显。
Conclusion Chronic effect, induced by liquid rocket propellant, was observed in our study.
完整性试验包括对推进剂和其它液体系统的泄漏检测。
The tests include the leak detection of liquid propellant and other liquid systems.
研究了低温推进剂液体火箭发动机供应管道系统充填过程的建模问题。
The priming process of feed lines of cryogenic propellant liquid rocket engines was studied.
以液氧加注控制系统为例，介绍液体运载火箭低温推进剂加注控制所采用的两级分布式系统。
The two level distributed control system for cryogenic propellant loading is introduced, taking the Lox loading control system for example.
以液氧加注控制系统为例，介绍液体运载火箭低温推进剂加注控制所采用的两级分布式系统。
The two level distributed control system for cryogenic propellant loading is introduced, taking the Lox loading control system for example.
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