1) HTPB composite propellant
HTPB复合推进剂
1.
The change rule of mechanical property of HTPB composite propellant with test time was studied by humidity test.
通过常温湿度试验,研究了HTPB复合推进剂力学性能随试验时间的变化规律。
2) AP/HTPB composite solid propellant
AP/HTPB固体复合推进剂
1.
Preparation of ferrocene grafted SBA-15 and its catalysis on AP/HTPB composite solid propellant;
二茂铁功能化SBA-15的制备及其对AP/HTPB固体复合推进剂燃烧催化作用研究
3) 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。
4) HTPB/AP propellant
HTPB/AP推进剂
5) 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。
补充资料：[3-(aminosulfonyl)-4-chloro-N-(2.3-dihydro-2-methyl-1H-indol-1-yl)benzamide]
分子式：C16H16ClN3O3S
分子量：365.5
CAS号：26807-65-8
性质：暂无
制备方法：暂无
用途：用于轻、中度原发性高血压。
分子量：365.5
CAS号：26807-65-8
性质：暂无
制备方法：暂无
用途：用于轻、中度原发性高血压。
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