1) hydroxy terminated polybutadiene propellant (HTPB)
丁羟推进剂(HTPB)
2) 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。
3) HTPB/AP propellant
HTPB/AP推进剂
4) AP/HTPB propellant
AP/HTPB推进剂
1.
Effect of dendritic nano-crystalline Co on combustion properties of AP/HTPB propellant;
树枝状纳米钴微晶对AP/HTPB推进剂性能的影响
2.
Effect of nano Ni/CNTs on thermal decomposition and combustion properties of AP/HTPB propellants;
纳米Ni/CNTs对AP/HTPB推进剂热分解及燃烧性能的影响
3.
The catalytic performance of nano Cu/CNTs in the thermal decomposition and combustion of AP/HTPB propellant was investigated.
研究了纳米Cu/CNTs对AP/HTPB推进剂热分解和燃烧过程的催化作用,结果表明:纳米Cu/CNTs能显著降低AP/HTPB推进剂的热分解峰温,并使总表观分解热明显增大,且对AP/HTPB推进剂燃烧有良好的催化效果,能显著提高推进剂的燃速,降低压强指数。
6) HTPB propellant
丁羟推进剂
1.
Study on the adjustment method of HTPB propellant binder matrix structure;
丁羟推进剂粘合剂网络结构调控方法探讨
2.
Study on the interfacial acid-base function of HTPB propellant components
丁羟推进剂组分间界面酸碱作用研究
3.
Applying burning-rate catalysts is one of optimal approaches to regulate the burning rate of HTPB propellant.
使用燃速催化剂是调节丁羟推进剂燃速的最佳途径之一。
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