bipropellant是什么意思   bipropellant怎么读

英式:[bɪprə'pelənt]    美式:[bɪprə'pelənt]

bipropellant单词基本解析:

n.& adj.二元推进剂(的),二元燃料(的)

bipropellant变化用词:



bipropellant英英释义:

bipropellant中文词源:

bipropellant用法和例句:

bipropellant


DSMC simulation of nozzle flow of bipropellant attitude control engine

DSMC法模拟双组元姿控发动机喷管流动


To understand characteristics of micro-thruster, ground-experimental apparatus of bipropellant micro-thruster and data acquisition system were established.

为研究微小推力室的工作特点,建立了双组元微小推力室的地面实验装置和数据采集系统。


bipropellant liquid rocket motor

二元推进剂液体火箭发动机


bipropellant rocket

二元燃料火箭发动机


Louis Larosiliere, Ron Litchford, Jeng San-Mou.Hypergolic Bipropellant Spray Combustion and Flow Modelling in Rocket Engines. AIAA 90-2238.

刘昌国.高比冲性能双组元远地点火箭发动机研究.卫星推进技术研讨会论文集,2002.11.


rocket bipropellant

双元火箭燃料


DSMC SIMULATION OF PLUME BACKFLOW FROM BIPROPELLANT ATTITUDE CONTROL ENGINE

双组元姿控发动机反流特性的DSMC模拟


NUMERICAL SIMULATION ON CHEMICAL REACTING FLOW OF BIPROPELLANT ALTITUDE CONTROLLING THRUSTER NOZZLE

双组元姿控发动机喷管化学反应流场数值模拟


bipropellant propulsion

双组元推进


bipropellant liquid apogee motor

双组元液体推进剂远地点发动机


Design Methods of Bipropellant Liquid Apogee Rocket Engine Turbulent Flow Annulus

双组元液体远地点火箭发动机扰流环的设计方法研究


bipropellant rocket engine

双组元火箭发动机


Rocket motor test shows that the new UDMH/NTO bipropellant can satisfy the requirement of gel propellant of rocket motor design.

发动机试验表明:新的UDMH/NTO双组元凝胶体系能够满足发动机设计对凝胶推进剂的要求。


Schindler,R.C. and Schoenmant,L.,Development of a Five-Pound Thrust Bipropellant Engine,J. Spacecraft,Vol.13.No.7,pp.435-442,1976.

叶威廷,“喷流孔径对冲击雾化混合分布之影响”,成功大学航太所硕士论文,九十五学年度。


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。


Louis Larosiliere , Ron Litchford , San-Mou Jeng. Hypergolic Bipropellant Spray Combustion and Flow Modeling in Rocket Engines[R]. AIAA 90-2238.

庄逢辰.液体火箭发动机喷雾燃烧的理论、模型及应用[M].长沙:国防科技大学出版社,1995,2.


The bipropellant gas-liquid coaxial orifice-swirl injector has great effects on the high-frequency combustion instability of the LOX/kerosene staged combustion cycled engine.

气液同轴直流离心式喷嘴对补燃发动机燃烧室高频燃烧稳定性有显著影响。


Keywords liquid propellants;density specific impulse;monopropellant;bipropellant;atomic propellant;

液体推进剂;密度比冲;单组元推进剂;双组元推进剂;原子推进剂;


Application of New Chamber Materials in Low Thrust Bipropellant Thruster for Spacecrafts

燃烧室新材料在卫星双组元低推力发动机上的应用


Technology for space chemical propulsion includes bipropellant propulsion, monopropellant propulsion and micropropulsion.

空间化学推进技术包括双组元推进、单组元推进和微推进技术。


Green Hypergolic Bipropellant Using Hydrogen Peroxide as an Oxidant

绿色过氧化氢双组元自燃推进剂


self-igniting bipropellant

自燃双组分推进剂


NUMERICAL SIMULATION OF STABLE COMBUSTION PROCESS IN EARTH STORABLE BIPROPELLANT ROCKET ENGINE

自燃推进剂火箭发动机稳态燃烧过程的数值模拟


Keywords hydrogen peroxide;bipropellant;hypergolic characteristic;ignition delay;

过氧化氢;双组元推进剂;自燃特性;点火延迟期;


Research on the High Specific Impulse Bipropellant Liquid Apogee Engine

高比冲双组元液体远地点火箭发动机研究