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首页> 外文期刊>Journal of propulsion and power >Enhancing Composite Solid Propellent Burning Rates with Potassium Doped Ammonium Perchlorate-Part Ⅰ
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Enhancing Composite Solid Propellent Burning Rates with Potassium Doped Ammonium Perchlorate-Part Ⅰ

机译:掺钾高氯酸铵提高复合固体推进剂的燃烧速度(Ⅰ)

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摘要

The objective of this paper is to understand the observed changes in behavior of ammonium perchlorate deflagration characteristics reported in literature, when it is doped with potassium. Successive recrystallization is employed to dope potassium into ammonium perchlorate. This paper, through various recrystallization techniques, conclusively puts an end to doubts regarding the actual process of acquisition of potassium by ammonium perchlorate. It is concluded that the increase in the potassium content in ammonium perchlorate is due to the filter used during recrystallization process. From the experiments conducted to obtain the deflagration rates of ammonium perchlorate, it is observed that potassium doped ammonium perchlorate has higher burning rates and also a higher low-pressure deflagration limit. As potassium doped is within the ammonium perchlorate crystal, thermal conductivity and specific heat values for ammonium perchlorate with various percentages of potassium are obtained. These values are incorporated into the computational studies on ammonium perchlorate. The computational studies performed in this paper are not intended to reproduce the experimental results but to illustrate the various features of the potassium doped ammonium perchlorate deflagration. With these computational studies, the observed burning rate increase and low-pressure deflagration limit increase of ammonium perchlorate with doped potassium are explained.
机译:本文的目的是了解文献报道的高氯酸铵掺钾时爆燃特性的变化。连续重结晶用于将钾掺杂成高氯酸铵。本文通过各种重结晶技术,最终结束了对高氯酸铵获取钾的实际过程的怀疑。结论是高氯酸铵中钾含量的增加归因于重结晶过程中使用的过滤器。从为获得高氯酸铵的爆燃率而进行的实验中,可以看出掺杂钾的高氯酸铵具有更高的燃烧率以及更高的低压爆燃极限。由于掺杂的钾在高氯酸铵晶体中,因此可以得到钾含量不同的高氯酸铵的热导率和比热值。这些值被纳入高氯酸铵的计算研究中。本文进行的计算研究并非旨在复制实验结果,而是要说明掺钾的高氯酸铵爆燃的各种特征。通过这些计算研究,解释了观察到的掺杂钾的高氯酸铵的燃烧速率增加和低压爆燃极限增加。

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  • 来源
    《Journal of propulsion and power》 |2014年第2期|277-284|共8页
  • 作者单位

    Indian Institute of Technology Madras, Chennai 600 036, India,Department of Aerospace Engineering;

    Indian Institute of Technology Madras, Chennai 600 036, India,Department of Aerospace Engineering;

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  • 正文语种 eng
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