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Aluminum agglomeration of AP/HTPB composite propellant

机译:AP / HTPB复合推进剂的铝凝聚

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Aluminum (Al) powder agglomeration is one of the main reasons for the degradation in the performance of aluminized solid propellant rockets and so, understanding the combustion behavior of aluminum in solid propellants is of great importance. In this work, a laser ignition test bench was used to study the behavior of Al on the burning surface of an aluminum/ammonium perchlorate/hydroxyl-terminated polybutadiene composite propellant, under atmospheric pressure. Based on the images captured by a high-speed camera, the agglomeration process and behavior of the agglomerates were analyzed in detail. The size distribution and speed of motion of the agglomerates away from the burning surface were also considered. Results show that the formation of an agglomerate on the burning surface from multiple aluminum particles include three stages: accumulation, aggregation, and agglomeration. Local ignition promotes the collapse of the aggregate into a spherical agglomerate. Before detachment, the agglomerates often roll around on the burning surface and pick up more aluminum, promoting self-growth. The interesting phenomenon of an agglomerate droplet rupturing and ejecting liquid alumina on the burning surface was clearly captured for the first time. This is believed to indicate the heterogeneous composition characteristics of the agglomerate. The transformation of the polar oxide cap on one part of the agglomerate surface into an alumina shell that fully covers the droplet surface was also captured for the first time. The agglomerates have different shapes, diameters, and velocities when they leave the burning surface. The formation of non-spherical agglomerates consisting of more than one aluminum droplet is ascribed to the propellant microstructure. The 400 agglomerates that were counted had diameters that ranged from 51 mu m to 815 mu m and the majority of them (nearly 98%) were below 400 mu m. The velocities of motion of 176 agglomerates exhibited great dispersion, with the maximum and minimum velocity being 196 cm/s and 13 cm/s, respectively. In general, the moving velocities of the agglomerates decreased with increasing diameter.
机译:铝(Al)粉末聚集是铝化固体推进剂火箭的性能下降的主要原因之一,因此了解铝中铝的燃烧行为具有重要意义。在这项工作中,使用激光点火试验台在大气压下研究Al在铝/氢铵/羟基封端的聚丁二烯复合推进剂的燃烧表面上的行为。基于由高速摄像机捕获的图像,详细分析附聚处理和附聚物的特征。还考虑了远离燃烧表面的附聚物远离燃烧表面的尺寸分布和运动速度。结果表明,从多个铝颗粒的燃烧表面上形成凝聚物包括三个阶段:积累,聚集和附聚。局部点火促进聚集体的坍塌成球形凝聚。在脱离之前,聚集体经常在燃烧的表面上滚动并拿起更多铝,促进自我生长。第一次清楚地捕获燃烧表面上的凝聚液滴破裂和喷射液氧化铝的有趣现象。据信这表示附聚物的异质组合物特征。也首次捕获了将聚集表面的一部分氧化物帽对氧化铝壳的一部分转化为完全覆盖液滴表面的氧化铝壳。当它们离开燃烧表面时,附聚物具有不同的形状,直径和速度。由一个以上的铝液滴组成的非球形附聚物的形成归因于推进剂微观结构。计数的400个附聚物的直径为51μm至815 mu m,其中大部分(近98%)低于400 mu m。 176个附聚物的运动速度表现出极大的分散体,其最大和最小速度分别为196cm / s和13cm / s。通常,聚集体的移动速度随着直径的增加而降低。

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