1.
bipropellant liquid apogee motor
![点击朗读](/dictall/images/read.gif)
双组元液体推进剂远地点发动机
2.
bipropellant rocket
![点击朗读](/dictall/images/read.gif)
双元液体推进剂火箭发动机
3.
bipropellant liquid rocket motor
![点击朗读](/dictall/images/read.gif)
二元推进剂液体火箭发动机
4.
Research and Manufacture of Red Fuming Nitric Acid/ UDMH Gel Bipropellant
![点击朗读](/dictall/images/read.gif)
红烟硝酸/偏二甲肼凝胶双组元推进剂研制
5.
Study on Curing System of Four-components HTPB Composite Propellants;
![点击朗读](/dictall/images/read.gif)
丁羟四组元复合固体推进剂固化体系研究
6.
NIRS Rapid Analysis of Composition and Character of Liquid Propellant
![点击朗读](/dictall/images/read.gif)
近红外光谱法快速分析液体推进剂组成和性质
7.
Investigation on the New Borate Ester Bonding Agents for the High Energy Four Groups Hydroxy-Terminated Polybutadiene Propellant;
高能丁羟四组元复合固体推进剂用新型硼酸酯键合剂研究
8.
Gaseous, liquid, or slurry propellants may be used in various combinations.
![点击朗读](/dictall/images/read.gif)
气态,液体或胶状推进剂可能用于各种不同组合中。
9.
Study on the Software of Configuration Analysis of Liquid Propellant Space Propulsion Systems;
液体推进剂空间推进系统构型分析软件研究
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.
Research on Two-Parameter Fracture Criterion of Composite Solid Propellants
![点击朗读](/dictall/images/read.gif)
复合固体推进剂双参数断裂准则研究
12.
The liquids employed for rocket propulsion are called propergols.
![点击朗读](/dictall/images/read.gif)
用于火箭发动机的液体称为液体火箭推进剂。
13.
Current Situation of Underwater Chemical-propellant
![点击朗读](/dictall/images/read.gif)
国外水下液体化学推进剂的研究现状
14.
Study on Properties of Series Pulse Electrical Ignition of Liquid Propellant Spray
![点击朗读](/dictall/images/read.gif)
液体推进剂液雾序列脉冲电点火特性研究
15.
Progress in combustion characteristic research of liquid rocket gelled propellants
![点击朗读](/dictall/images/read.gif)
液体火箭凝胶推进剂燃烧特性研究进展
16.
Research on 1N mono-propellant rocket engine with low freezing point propellant
![点击朗读](/dictall/images/read.gif)
低冰点推进剂1N单组元发动机技术研究
17.
Experimental Research of Constitutive Relationship of DB Solid Propellant Grain
![点击朗读](/dictall/images/read.gif)
双基固体推进剂药柱本构关系的实验研究
18.
It is reasonable that this result should be generally applicable also to liquid-propellant rockets.
这个结果通常也应适用于液体推进剂火箭。