1)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。
英文短句/例句
1.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
2.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
3.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
4.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
5.Digital Signal Processing System Design of Low-temperature Propellant Level Based on DSP;基于DSP的低温推进剂加注液位检测和信号处理系统设计
6.Experimental Study and Theoretical Analysis Method Investigation on Natural Circulation Precooling of Cryogenic Propellant Rocket Engine System;低温推进剂火箭发动机循环预冷实验和分析方法研究
7.Numerical simulation on unsteady process in chilldown of cryogenic propellant transfer system低温推进剂输送系统循环预冷非稳态数值模拟研究
8.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
9.Transient viscoelastic characteristics of NEPE propellant at low temperatureNEPE推进剂低温瞬态的粘弹特性
10.Research Development on Cryogenic Solid Propulsion Technology低温固体推进(CSP)技术研究进展
11.Pasty Propellant Flame Temperature Measurement Based on Image Processing基于图像处理的膏体推进剂火焰测温
12.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
13.Study and Test of New Cold Flow Improvers for Diesel Fuel;新型柴油低温流动改进剂的实验研究
14.Progress in the research of gold nano-particles catalysts for CO oxidation in low temperatureCO低温氧化纳米金催化剂研究进展
15.A STUDY OF COLD FLOW IMPROVERS FOR SOYBEAN BIODIESEL FUEL大豆油生物柴油低温流动改进剂研究
16.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
17.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
18.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
相关短句/例句
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
3)cryogenic propellant tank低温推进剂贮箱
1.Distributed parameter numerical simulation for the transients of cryogenic propellant tank pressurization system(Ⅰ)Finite volume model of tank;低温推进剂贮箱增压系统分布参数数值仿真(Ⅰ)贮箱的有限体积模型
4)cryogenic propellant[航]低温推进剂
5)Cryogenic propellant rocket engine低温推进剂火箭发动机
6)High temperature propellant高温推进剂
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。
