1.
In combination with the actual development state abroad, the main research orientations and the key points of high energy solid propellant technology for the future were put forwards.
结合国外发展现状,提出了高能固体推进剂技术未来发展的主要方向及重点。
2.
Virtual Machine Tool Technology for Solid Rocket Propellant
用于固体火箭推进剂的多功能集成虚拟机床技术
3.
Design of Mechanics Response Prediction System for High Energy Solid Propellants
高能固体推进剂力学性能预示系统设计
4.
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
5.
Elimination of Toxic Materials and Solvents from Solid Propellant Components (PP1058) ^Annual technical rept. For FY 1998
固体推进剂组分中的毒性材料和溶剂的去除/1998财年年度技术报告
6.
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
7.
Using parabolic trajectory of ballistic missile, surface to air missile with solid propellant can realize the aim of lesser weight and farther range.
地空导弹采用弹道导弹的抛物弹道技术，能够实现应用固体推进剂达到低质量远射程的目标。
8.
Research Development on Cryogenic Solid Propulsion Technology
低温固体推进(CSP)技术研究进展
9.
Study on EO-THF Copolymer Reference Materials Used in Solid Propellant;
高能固体推进剂用聚（环氧乙烷—四氢呋喃）标准物质的研究与制备
10.
Composite solid propellant slurry is a viscous fluid with high percentage of solid particles.
复合固体推进剂药浆是固体粒子含量很高的粘性流体。
11.
Research on the Method to Predict the Quasi-static Mechanical Property for Solid Propellant;
固体推进剂准静态力学性能预测方法研究
12.
The Effect of Poisson Rate on Mechanics Properties of Solid Propellant
泊松比对固体推进剂药柱力学性能的影响
13.
Abstract: Using parabolic trajectory of ballistic missile, surface to air missile with solid propellant can realize the aim of lesser weight and farther range.
文摘:地空导弹采用弹道导弹的抛物弹道技术，能够实现应用固体推进剂达到低质量远射程的目标。
14.
Application Progress of Metal Fuels in Solid Propellants
金属燃料在固体推进剂中的应用进展
15.
The applicated progress of catalyst technology of solid acid;
固体酸催化剂技术应用的进展及主要问题
16.
Research Progress on High Precision Planarization Technology for Solid Surface
固体表面高精密平面化技术研究进展
17.
The Study on Mutilple Starts of Pasty Propellant Rocket
膏体推进剂火箭发动机多次启动技术研究
18.
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