1)low freezing point propellant低冰点推进剂
1.The formulas were fitted about the relation between temperature and some attributes of the low freezing point propellant (DT-3/MON-25).本文以挤压式液体火箭发动机和低冰点推进剂为研究对象,以工程研制为背景,对小型的双模式空间液体火箭发动机系统进行建模及其静态特性及动态特性的研究,对低冰点推进剂(DT-3/MON-25)在低温时温度对其性能影响的关系式进行了拟合,对低冰点推进剂在入口温度较低时以及不同工况时对火箭发动机的性能影响进行了仿真研究,并且根据仿真结果对推进系统在不同的推进剂温度环境下的各种性能进行了比较和分析。
2.In view of the importance of low freezing point propellant in performance research of liquid-propellant rocket engine,the starting process and static-state process of a liquid rocket engine with MON-25/DT-3 low freezing point propellant were studied.针对低冰点推进剂在液体火箭发动机性能研究中的重要性,对使用MON-25/DT-3组合的低冰点推进剂液体火箭发动机的启动过程及稳态过程进行研究。
英文短句/例句
1.Research on 1N mono-propellant rocket engine with low freezing point propellant低冰点推进剂1N单组元发动机技术研究
2.The Research on Influence of Low Freezing Point Propellant on Performance of Liquid-propellant Rocket Engine低冰点推进剂对液体火箭发动机性能影响研究
3.Research on Modeling and Simulation of Liquid-propellant Rocket Engines with Low Freezing Point Propellant for Attitude and Orbit Control Using Two Mode低冰点双模式姿轨控推进系统建模与仿真研究
4.freezing point depression凝冻点（冰点）降低
5.Study on the Formulation of Low Burning Rate HTPB Propellant with RDX含RDX低燃速丁羟推进剂的配方研究
6.Propellant inlet temperature control for cryogenic rocket engine tests低温发动机试验推进剂入口温度控制
7.Transient viscoelastic characteristics of NEPE propellant at low temperatureNEPE推进剂低温瞬态的粘弹特性
8.Progress of Study on Transpiration Control Technology for Orbit Long-term Applied Cryogenic Propellant低温推进剂长时间在轨的蒸发量控制技术进展
9.bipropellant liquid apogee motor双组元液体推进剂远地点发动机
10.The comparison between the solid bipropellant firing results and the monopropellant firing results appears to be quite good.固体二元推进剂和单元推进剂的点火试验结果是很相近的。
11." Antifreeze： Any substance that lowers the freezing point of water, protecting a system from the ill effects of ice formation."防冻剂:降低水之凝固点的物质，能够保护系统免受冰冻之害。
12.The Software Designing and Realizing of Liquid Level Detecting System;低温推进剂液位检测系统软件设计与实现
13.Research on Thermal-mechanical Coupled Analysis of Launch Vehicle Cryogenic Tanks航天运载器低温推进剂贮箱热力耦合分析研究
14.Preliminary Study of Properties of High Energy and Low Signature CL-20 Based Solid PropellantsCL-20基高能低特征信号推进剂性能初探
15.Numerical simulation of slug bubble formation in a vertical cryogenic propellant pipe低温推进剂弹状汽泡形成过程的数值模拟研究
16.molal depression constant克分子冰点降低常数
17.A substance, often a liquid such as ethylene glycol or alcohol, mixed with another liquid to lower its freezing point.防冻剂，防冻液，抗凝剂一种物质，通常是液体，如乙二醇或酒精，和另一种液体混合来降低冰点
18.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
相关短句/例句
freezing point depressant冰点降低剂
3)Cryogenic propellant低温推进剂
1.Numerical simulation of slug bubble formation in a vertical cryogenic propellant pipe低温推进剂弹状汽泡形成过程的数值模拟研究
2.The key design parameters such as tank material selection, cryogenic propellant caused structure thermo stress and heat insulation structure are discussed.从低温表面张力贮箱的材料选择、低温推进剂引起的热应力及隔热层结构形式等方面进行了初步探讨。
4)Propellant ignition推进剂点火
5)cryoscopic solvent冰点降低溶剂
6)cryogenic liquid propellant低温液体推进剂
1.Numerical simulation of filling pipe of cryogenic liquid propellant;低温液体推进剂充填管路的数值模拟
延伸阅读
低温推进剂分子式：CAS号：性质：在标准大气压力下，沸点低于200K的液体推进剂。亦称深冷推进剂，如液氧、液氢、液氟等。应贮存于绝热良好的容器中，以尽量减少其挥发损失。主要用于航天运载火箭。
