首页> 外文会议>Seminar on New Trends in Research of Energetic Materials;NTREM '11 >Ageing behaviour of rocket propellant formulations with ADN as oxidiser
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Ageing behaviour of rocket propellant formulations with ADN as oxidiser

机译:以ADN为氧化剂的火箭推进剂配方的老化行为

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Characteristics and ageing of several ADN containing composite rocket propellant formulations were investigated. Binders have been GAP cured with BPS (bis-propargyl succin-ate) and Desmophene~(tm) D2200 cured with Desmodur~(tm) N3400. Comparisons are made with AP analogues, with formulations where HMX has replaced Al, and with typical HTPB/Al/AP formulations. GAP-BPS/ADN/HMX and GAP-BPS/ADN/Al have low strength and low strain capability compared to HTPB/AP/Al-based propellants. Desmophene™ -bonded materials (ADN/Al, AP/Al, AP/HMX) have lower strain capabilities but higher strength values. The effectiveness of a bonding agent for ADN named HX-880 was studied, but a negligible effect on the mechanical properties was found and incompatibility with ADN was observed. SEM analyses of the GAP-BPS/ADN formulations showed the presence of voids and a high porosity of the propellant formulations. With ageing the ADN formulations showed remarkable chemical decomposition (mass loss measurements evidenced an autocatalytic behaviour at above 60°C) and, more severe, extended dewetting between matrix and ADN prills. The glass transition temperatures determined by DMA for the GAP- and Desmophene™-based formulations are about half as negative as the values of the AP/Al/HTPB-based propellants. The dynamic mechanical behaviour of the ADN formulations is different to the HTPB-based materials. Only one obvious peak in the loss factor curve was found instead of two. The filler (HMX or Al), oxidisers (AP or ADN) and curing agents (BPS or N3400) have influences on the glass transition temperature, peak broadness and apparent activation energy of the shift of peak temperature. The total peak of the GAP formulations is broader than the one of the Desmophene™ formulations. Lowering of T_g by the addition of AP was found. The fact that systematically the glass transition temperature is lower with AP compared to the ADN-based formulations can be explained with a stronger interaction between ADN and binder chains than between AP and binder chains.
机译:研究了几种含ADN的复合火箭推进剂配方的特性和老化。粘合剂已用BPS(双-炔丙基琥珀酸酯)和Desmophene®T2200用Desmodur®N3400固化。与AP类似物,HMX替代Al的配方以及典型的HTPB / Al / AP配方进行了比较。与基于HTPB / AP / Al的推进剂相比,GAP-BPS / ADN / HMX和GAP-BPS / ADN / Al具有低强度和低应变能力。 Desmophene™粘结材料(ADN / Al,AP / Al,AP / HMX)具有较低的应变能力,但强度值较高。研究了一种名为HX-880的ADN粘合剂的有效性,但发现其对机械性能的影响可忽略不计,并观察到与ADN的不相容性。 GAP-BPS / ADN配方的SEM分析表明,推进剂配方中存在空隙和高孔隙率。随着时间的流逝,ADN配方会表现出显着的化学分解作用(质量损失测量结果表明,在60°C以上时会发生自催化行为),并且基质和ADN颗粒之间的脱湿现象更加严重。由DMA确定的基于GAP和Desmophene™的配方的玻璃化转变温度大约为基于AP / Al / HTPB的推进剂值的一半。 ADN配方的动态力学行为不同于基于HTPB的材料。在损耗因子曲线中仅发现一个明显的峰,而不是两个。填料(HMX或Al),氧化剂(AP或ADN)和固化剂(BPS或N3400)会影响玻璃化转变温度,峰宽和峰温变化的表观活化能。 GAP制剂的总峰比Desmophene™制剂之一的峰更宽。发现通过添加AP降低了T_g。与基于ADN的配方相比,使用AP系统地玻璃化转变温度更低的事实可以解释为,ADN与粘合剂链之间的相互作用比AP与粘合剂链之间的相互作用更强。

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