1) EMCDB propellant
EMCDB推进剂
1.
The experiment, applied to study the curing catalysis of combustion catalysis for polyurethane EMCDB propellant, was designed, the catalytic activity of eight Pb salts and four Cu salts was compared, the Pb salts and Cu-salts, which could be used as combustion catalyst ingredient of EMCDB propellant, were selected.
设计了一种研究燃烧催化剂对 EMCDB推进剂交联固化反应催化作用的实验方法 ,比较了十多种铅盐、铜盐对交联固化反应催化活性的强弱 ,筛选出了可用作粒铸 EMCDB推进剂燃烧催化剂的铅盐、铜盐。
2.
In this paper, granule-casting process had been first successfully applied to the shapingof EMCDB propellant.
本论文首次将粒铸工艺成功应用于EMCDB推进剂成型。
2) propellant
[英][prə'pelənt] [美][prə'pɛlənt]
推进剂
1.
An Analysis of Propellant Storage Life and Reliability Based on Gel Fraction;
基于凝胶百分数的推进剂贮存寿命及其可靠性分析
2.
Influence of Surface Coating of RDX Fillers on the Safe Properties of HTPB Propellant;
丁羟推进剂RDX填料表面包覆对其安全性能的影响研究
3.
Performance Rearch of Metallized Gelled Propellant;
金属化胶体推进剂性能研究
3) NEPE propellant
NEPE推进剂
1.
Effects of composite burning-rate modifiers on combustion properties of NEPE propellant under high pressure;
复合燃速调节剂对NEPE推进剂高压燃烧性能的影响
2.
Effect of tensile rate on mechanical properties of NEPE propellant;
拉伸速率对NEPE推进剂力学性能的影响
3.
Effect of ingredient migration on interface bonding properties of NEPE propellant;
组分迁移对NEPE推进剂界面粘接性能的影响
4) HTPB propellant
HTPB推进剂
1.
Investigation on prediction model for storage life of HTPB propellants;
HTPB推进剂贮存期预估模型研究
2.
Mechanism of influence of active groups in binder on mechanical properties of HTPB propellants
黏合剂活性基团对HTPB推进剂力学性能的影响机制
3.
To improve the performance of the propellant,energy properties,mechanical properties and combustion properties of HTPB propellants were studied.
为进一步提高HTPB推进剂的能量水平,从理论和实验两个方面研究了固体组分含量对HTPB推进剂的能量性能、燃烧性能和力学性能的影响。
5) propellants
推进剂
1.
The TNAZ is especially suitable for the application as a component of solid propellants and explosives.
1,3,3-三硝基氮杂环丁烷(TNAZ)是一种新型含能材料,由于其具有熔点低、感度低、能量高、热稳定好、易与其他含能材料形成低共熔物等优点,特别适于用作固体推进剂和炸药组分。
2.
In order to investigate the characters of high energy solid propellants initiated by shock waves,the Lagrange analytical experiment equipment was designed.
为了研究高能固体推进剂的冲击起爆行为,对推进剂进行了冲击加载下的拉氏分析实验。
3.
The heating layer thickness of pasty propellants near wall surfaces increases with the augmentation of caliber and decreases with the increase of velocity.
为研究膏体推进剂供给管道受热后对推进剂的热稳定性及流动性能的影响,针对膏体推进剂在热管道内的流动情况,结合不可压缩N-S方程及幂律本构关系进行建模与仿真,获得膏体推进剂在热管道内的流动特性,分析了其流动时的受热状况。
6) CMDB propellant
CMDB推进剂
1.
The application of the high energy density material(HEDM) CL-20,DNTF and FOX-12 in CMDB propellant were studied.
首次在螺压CMDB推进剂中对CL-20、DNTF、FOX-123种高能量密度材料进行了应用研究,发现这3种材料能在螺压工艺中安全地制成样品。
2.
Various technique approaches, by which the mechanical property of CMDB propellant would be improved, are summarized.
讨论了脱湿对硝胺CMDB推进剂力学性能的影响和脱湿机理,总结了改善硝胺CMDB推进剂力学性能的各种技术途径,认为键合剂是增强硝胺CMDB推进剂界面粘接、提高力学性能的有效和现实的技术途径,综述了键合剂的主要种类及其最新应用研究进展;分析了键合剂在硝胺CMDB推进剂中应用的难点和键合剂选择原则,表明在硝胺CMDB推进剂中应用键合剂是必要和可行的。
3.
The mechanical sensitivity and combustion properties of CMDB propellant using phase stabilized ammonium nitrate(PSAN) as oxidizer were investigated through the burning rate, impact sensitivity and friction sensitivity measurements.
结果表明,PSAN可改善CMDB推进剂的机械感度;用PSAN作氧化剂,其推进剂的燃速低于RDX作氧化剂的燃速,压强指数高于后者的压强指数;1～5MPa压力范围内随PSAN在配方中含量的增加,推进剂的燃速降低,压强指数升高。
补充资料：固液混合火箭推进剂(见火箭推进剂)
固液混合火箭推进剂(见火箭推进剂)
solid-liguid hybrid rocket propellant
guye hunhe huoiian tui)in)i固液混合火箭推进剂(s olid一Iiguid hy-brid rocket proPellant)见火箭推讲齐，}_
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条