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Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives

机译:使用纳米级添加剂调整复合推进剂的高原燃烧速率

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摘要

Composite propellants are composed of a solid oxidizer that is mixed into a hydrocarbon binder that when polymerized results in a solid mass capable of self-sustained combustion after ignition. Plateau propellants exhibit burning rate curves that do not follow the typical linear relationship between burning rate and pressure when plotted on a log-log scale, and because of this deviation their burning behavior is classified as anomalous burning. It is not unusual for solid-particle additives to be added to propellants in order to enhance burning rate or other properties. However, the effect of nano-size solid additives in these propellants is not fully understood or agreed upon within the research community. The current project set out to explore what possible variables were creating this result and to explore new additives.This thesis contains a literature review chronicling the last half-century of research to better understand the mechanisms that govern anomalous burning and to shed light on current research into plateau and related propellants. In addition to the review, a series of experiments investigating the use of nanoscale TiO2-based additives in AP-HTPB composite propellants was performed. The baseline propellant consisted of either 70% or 80% monomodal AP (223 ?m) and 30% or 20% binder composed of IPDI-cured HTPB with Tepanol. Propellants? burning rates were tested using a strand bomb between 500 and 2500 psi (34.0-170.1 atm).Analysis of the burning rate data shows that the crystal phase and synthesis method of the TiO2 additive are influential to plateau tailoring and to the apparent effectiveness of the additive in altering the burning rate of the composite propellant. Some of the discrepancy in the literature regarding the effectiveness of TiO2 as a tailoring additive may be due to differences in how the additive was produced. Doping the TiO2 with small amounts of metallic elements (Al, Fe, or Gd) showed additional effects on the burning rate that depend on the doping material and the amount of the dopant.
机译:复合推进剂由混合到烃粘合剂中的固体氧化剂组成,当聚合时会产生一种固体物质,该固体物质在点火后能够自我持续燃烧。当以对数-对数标度绘制时,高原推进剂的燃烧速率曲线不遵循燃烧速率与压力之间的典型线性关系,由于这种偏差,它们的燃烧行为被归类为异常燃烧。固体颗粒添加剂被添加到推进剂中以提高燃烧速率或其他性能并不少见。然而,纳米粉末固体添加剂在这些推进剂中的作用尚未得到研究界的充分理解或同意。当前的项目旨在探索产生此结果的可能变量并探索新的添加剂。本文包含对过去半个世纪的研究进行编年史的文献综述,以更好地了解控制异常燃烧的机制并阐明当前的研究进入高原和相关的推进剂。除了该综述之外,还进行了一系列实验,研究了在AP-HTPB复合推进剂中使用纳米级TiO2基添加剂。基准推进剂由70%或80%的单峰AP(223?m)和30%或20%的粘结剂组成,粘结剂由IPDI固化的HTPB和Tepanol组成。推进剂?使用在500至2500 psi(34.0-170.1 atm)之间的链弹测试了燃烧速率。燃烧速率数据的分析表明,TiO2添加剂的晶相和合成方法对高原剪裁和表面活性有影响。改变复合推进剂燃烧速率的添加剂。关于TiO2作为定制添加剂的有效性的文献中的某些差异可能是由于添加剂的生产方式不同所致。用少量金属元素(Al,Fe或Gd)掺杂TiO2对燃烧速率产生了其他影响,这取决于掺杂材料和掺杂剂的量。

著录项

  • 作者

    Stephens Matthew Aaron;

  • 作者单位
  • 年度 2009
  • 总页数
  • 原文格式 PDF
  • 正文语种 en_US
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