1) RDX-CMDB propellant
RDX-CMDB推进剂
1.
Determination on constant-volume combustion energy of 2-hydroxy-3,5-dinitropyridine lead salt and its application in RDX-CMDB propellant;
2HDNPPb恒容燃烧能的测定及其在RDX-CMDB推进剂中的应用
2.
The thermal decomposition of RDX-CMDB propellants with burning rate catalysts [lead-gallate(GDPB),Cu(Ⅱ)-p-aminobenzoic acid(PAC) and carbon black(CB)] was investigated by pressure differential scanning calorimetry(PDSC).
用高压差示扫描量热仪(PDSC)研究了一种RDX-CMDB推进剂在所选用燃速催化剂(没食子高铅、对氨基苯甲酸铜和炭黑)作用下的热分解,并对比了纳米和非纳米催化剂对其热分解的影响。
2) 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。
4) AP/CMDB propellant
AP/CMDB推进剂
5) RDXXLDB propellant
RDX-XLDB推进剂
6) modified double base propellant(CMDB)
改性双基推进剂(CMDB)
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