1.
Rheological Study on the Crosslinking of NEPE Propellant
NEPE推进剂固化交联的流变学研究
2.
Study on Curing System of Four-components HTPB Composite Propellants;
丁羟四组元复合固体推进剂固化体系研究
3.
The final operation in propellant manufacture is the curing of the binder.
制造推进剂的最后操作是粘合剂的固化。
4.
Characterization, Prediction and Optimization of the Interfacial Adhesion of Composite Solid Propellant
复合固体推进剂界面粘结的预估、表征及优化
5.
Application Progress of Metal Fuels in Solid Propellants
金属燃料在固体推进剂中的应用进展
6.
THE WEIGHTED AVERAGE FUNCTIONALITY OF HTPB BINDER AND ITS CORRELATIVITY WITH THE BEST CURING PARAMETER OF SOLID PREPELLANTS
丁羟胶重均官能度及其与推进剂最佳固化参数相关性的研究
7.
SPIRBM (Solid Propellant Intermediate Range Ballistic Missile)
固体推进剂中程弹道导弹
8.
A mass of solid propellant.
块状燃料一块固体推进剂
9.
Research on the Micro-mechanics and Constitutive Relation for Solid Propellant;
固体推进剂细观力学与本构关系研究
10.
Study of shear experiment of solid propellant with alterable directions
固体推进剂的变角剪切力学试验研究
11.
Research on Two-Parameter Fracture Criterion of Composite Solid Propellants
复合固体推进剂双参数断裂准则研究
12.
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。
13.
Preparation of Novel Composite Combustion Catalyst Based on Carbon Nanotubes and Its Application in Solid Propellants;
新型碳纳米管基复合燃烧催化剂的制备及其在固体推进剂中的应用
14.
Some propellant droplets may not evaporate within the confines of the thrust chamber.
有些推进剂可能在推力室内并未汽化。
15.
Study on Applying of Assumption of Grain Crack with no Deformation
固体推进剂裂纹不变形假设使用条件的研究
16.
Researches on Combustion and Processes of High Boron Content Boron-Based Fuel-Rich Solid Propellants;
高含硼富燃固体推进剂工艺和燃烧性能研究
17.
Structural Reliability Analysis for Viscoelastic Materials of Solid Propellant;
固体推进剂类粘弹性材料结构可靠性分析
18.
The Analysis and Numeration of Solid Rocket Propellant's Finite Element Theory;
固体火箭推进剂有限元理论分析与计算