liquid propellant
英 [ˈlɪkwɪd prəˈpelənt]
美 [ˈlɪkwɪd prəˈpelənt]
网络 液体推进剂; 液体燃料
双语例句
- The missile'sfirst stage uses a liquid propellant;
导弹的第一段采用液体燃料推进剂； - Steady state fault detection and diagnosis of liquid propellant rocket engines based on decision tree method;
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。 - To verify the effectiveness of the control method, the digital simulation of controlling the variable thrust liquid propellant rocket engine with this controller is presented.
变推力液体火箭发动机可以满足这一要求，但当发动机的推力大范围变化时，发动机的动态特性随之变化，这使得简单的反馈控制难以满足控制要求。 - Based on the requirements for development of liquid propellant rocket engine and shaped charge warhead, the manufacturing technique of their key parts was researched.
结合液体火箭发动机和破甲弹的发展需求，将磨擦辅助精密电铸技术应用于其关键零件的制造。 - 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。 - A calculation of the wall temperature distribution in liquid propellant rocket engine chamber with milled grooves was completed by the aid of three-dimensional finite element method.
采用三维有限元模型对液体火箭发动机铣槽推力室进行了壁温分布计算。边界条件按一维经验公式处理。 - Glyoxal is prepared with waste liquid propellant HNO3-27S and ethanal.
利用报废的液体推进剂硝酸-27S和乙醛制备乙二醛。 - To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood. ( of non-living objects) the state of being free of pathogenic organisms.
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。 - Concrete steps and some effective measures for improving the liquid propellant rocket engine which is weak in the tangential mode of high frequency stability are also described in the paper.
根据所得结果，为此发动机中安装径向隔板的必要性提供了理论依据井对稳定性不佳的液体火箭发动机提出了具体改进步骤及一些有效措施。 - Bayesian Lower Limit of Life-time Reliability for Liquid Propellant Rocket Engine
液体火箭发动机寿命可靠性的贝叶斯下限 - NIRS Rapid Analysis of Composition and Character of Liquid Propellant
近红外光谱法快速分析液体推进剂组成和性质 - Particle Swarm Optimization Algorithm Based Damage-mitigating Control for Reusable Liquid Propellant Rocket Engine
基于粒子群算法的可重复使用液体火箭发动机减损优化问题研究 - The ground simulation test for gauging liquid propellant remaining on a satellite is introduced.
介绍了气体注入压力激励方法测量卫星液体推进剂剩余量地面模拟试验； - 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。 - It is important to study control of the combustion in bulk-loaded liquid propellant gun.
为开展整装式液体发射药火炮工作机理研究提供有益参考。 - Experiment method on mechanism of thrust of laser-induced ablation propulsion with liquid propellant
液体烧蚀激光推进推力形成机理实验方法 - Study on flow characteristic in bore in liquid propellant electrothermal chemical gun
液体工质电热化学炮膛内流动特征研究 - Study on Properties of Series Pulse Electrical Ignition of Liquid Propellant Spray
液体推进剂液雾序列脉冲电点火特性研究 - Effect of liquid propellant space engines system on centroid drift
液体推进剂空间发动机系统对质心漂移的影响 - Numerical Simulation of Pressure Oscillation in Combustion Chamber of Regenerative Liquid Propellant Gun
再生式液体发射药火炮燃烧室压力振荡数值仿真 - 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。 - 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 droplet distributing properties in atomization field of HAN based liquid propellant have been experimentally investigated by use of laser holographic system.
采用激光全息摄影系统，开展了HAN基液体发射药喷雾场颗粒分布特性的实验研究。 - The evolution of quality analysis for liquid propellant is reviewed.
对液体推进剂质量分析方法的发展进行了综述。 - A liquid propellant vapour detector based on the principle of photoionization has been designed.
根据光离子化检测原理，研制了液体推进剂蒸汽检测仪。 - The development approaches of various types of liquid propellant rocket engines are discussed.
对各种型式的液体火箭发动机的发展途径进行讨论。 - 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。 - 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 research results are of value to the analysis of interior ballistic process of regenerative liquid propellant guns.
研究结果对分析再生式液体发射药火炮内弹道过程有参考价值。 - 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。