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Wetting of oxidizer particles by binder and plasticizer molecules - microcalorimetry experiments and computer simulations

机译:粘合剂和增塑剂分子润湿氧化剂颗粒-微量热实验和计算机模拟

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Composite rocket propellants (CRP) contain oxidizer particles and fuel particles in an elastomeric binder matrix: The oxidizing agent is mostly ammonium perchlorate (AP) and the elastomer is hydroxyl terminated polybutadiene (HTPB) based polyurethane. The components differ widely in terms of crystallinity, thermal expansion behaviour and polarity. Especially, under broad temperature variations insufficient resilience leads to detachment or de-wetting of filler material from the binder. The ageing of such material was successfully characterized by DMA (dynamic mechanical analysis) measurements. The loss factor shows characteristic changes in shape and intensity. The shape of the loss factor is also determined by the intermolecular interactions between binder elastomer and filler materials. Also the transitions between non-glassy and glassy states of polymer binders and plasticizers are strongly determined by intermolecular interaction forces. This work intends to contribute to elucidating this aspect: Molecular dynamics simulations (MD) procedures are employed for a determination of binder-oxidizing agent interaction. MD is based on the approximation of atoms as point masses and point charges. Iterative solution of classical equations of motion with interatomic forces yields correct structure and energies within simulated volume elements. The procedure uses the crystal structure of the oxi-dant and the molecular topology of the elastomer as input parameters, at given temperature and pressure: First, sets of representative crystal surfaces are identified, which are then loaded with a bulk of adsorbate molecules, means binder and plasticizer molecules. From simulation runs at experimental conditions, the energy of interaction is extracted. Results are compared to those from solution microcalorimetry: This methods provides with the thermal response upon mixing AP powders with uncured HTPB, or plasticising agents as dioctyladipate (DOA), and azido-terminated glycidylazide polymer (GAP-A). Although originally designed for measurement of heats of solution, the setup is used to measure the heat of immersion within saturated solutions.
机译:复合火箭推进剂(CRP)在弹性体粘合剂基体中包含氧化剂颗粒和燃料颗粒:氧化剂主要是高氯酸铵(AP),弹性体是基于羟基封端的聚丁二烯(HTPB)的聚氨酯。组分在结晶度,热膨胀行为和极性方面差异很大。特别地,在宽的温度变化下,不足的回弹性导致填充材料从粘合剂上分离或去湿。此类材料的老化已通过DMA(动态机械分析)测量成功表征。损耗因子显示出形状和强度的特征变化。损耗因子的形状还取决于粘合剂弹性体和填充材料之间的分子间相互作用。聚合物粘合剂和增塑剂的非玻璃态和玻璃态之间的过渡也强烈地取决于分子间的相互作用力。这项工作旨在有助于阐明这一方面:分子动力学模拟(MD)程序用于确定粘合剂-氧化剂相互作用。 MD基于原子作为点质量和点电荷的近似值。具有原子间作用力的经典运动方程的迭代解可在模拟的体积元素内产生正确的结构和能量。该程序在给定的温度和压力下,使用氧化剂的晶体结构和弹性体的分子拓扑结构作为输入参数:首先,确定一组代表性的晶体表面,然后加载大量的吸附物分子,粘合剂和增塑剂分子。从实验条件下的模拟运行中,可以提取相互作用的能量。将结果与溶液微量量热法的结果进行比较:将AP粉与未固化的HTPB或增塑剂二辛基己二酸酯(DOA)和叠氮基封端的缩水甘油基叠氮化物(GAP-A)混合后,该方法可提供热响应。尽管最初设计用于测量溶液的热量,但是该设置用于测量浸入饱和溶液中的热量。

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