1) hydroxyl-terminated polyether(HTPE) propellant
HTPE推进剂
1.
The research process of hydroxyl-terminated polyether(HTPE) propellants,including the development and production of HTPE binders,comparison between HTPE and hydroxyl-terminated polybutadiene(HTPB),aging of HTPE propellants and improving on insensitive property of HTPE propellants were reviewed.
介绍了HTPE黏合剂的研制与生产,对比了HTPE推进剂与HTPB推进剂,并对HTPE推进剂的老化性能以及对其钝感性能的改进进行了说明。
2) HTPE binder
HTPE粘合剂
1.
Especially,the application features of HTPE binder for high-pressure operation and insensitive munitions needs,and its research significance are reviewed.
为探究固体推进剂粘合剂分子改性的发展需求和发展思路,总结了国外HTPE固体推进剂粘合剂的研究应用状况,分析了这种粘合剂所处的高分子化学发展环境及所涉及的一些前沿问题,重点评述了HTPE粘合剂推进剂适应高压强工作环境、满足钝感要求的应用特点和所采用的嵌段共聚分子设计技术的研究意义,以此提出固体推进剂粘合剂的一种发展途径。
3) 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
4) 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
5) 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。
6) 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。
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