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兵工学报 ›› 2013, Vol. 34 ›› Issue (9): 1072-1077.doi: 10.3969/j.issn.1000-1093.2013.09.003

• 研究论文 • 上一篇    下一篇

La0. 8Sr0. 2CoO3-δ的合成、表征及对硝胺改性双基推进剂的燃烧性能影响研究

卫芝贤1,2, 王雅乐1, 高原1, 刘吉平2,3, 左英英4   

  1. 1. 中北大学理学院, 山西太原030051; 2. 北京防护材料与技术研究所, 北京100072; 3. 北京理工大学材料学院, 北京100081; 4. 山西兴安化学工业集团有限责任公司, 山西太原030008
  • 收稿日期:2012-03-26 修回日期:2012-03-26 上线日期:2013-11-11
  • 作者简介:卫芝贤(1965—),女,教授,博士生导师。

Synthesis and Characteristics of La0. 8Sr0. 2CoO3-δand Its Effect on Combustion Property of Nitramine Modified Double-base Propellant

WEI Zhi-xian 1, 2, WANG Ya-le 1, GAO Yuan 1, LIU Ji-ping 2, 3, ZUO Ying-ying 4   

  1. 1. Science Institute, North University of China, Taiyuan 030051, Shanxi, China; 2. Beijing Institute of Protective Materials and Technology, Beijing 100072, China; 3. School of Materials Science and Engineering, Beijing Institute of Technology, Beijing 100081, China; 4. Shanxi Xing-An Chemical Industry Company, Taiyuan 030008, Shanxi, China
  • Received:2012-03-26 Revised:2012-03-26 Online:2013-11-11

摘要:

为探讨钙钛矿型氧化物对硝胺改性双基推进剂燃烧性能的影响,用硬脂酸凝胶燃烧法制备了钙钛矿型La0. 8Sr0. 2CoO3-δ,运用X 射线衍射(XRD)、扫描电镜(SEM)、傅里叶变换红外(FT-IR)光谱及光电子能谱(XPS)技术对所得粉体进行了表征,并用热重-差示扫描量热(TG-DSC) 技术研究了La0. 8Sr0. 2CoO3-δ对推进剂中主要组分黑索今( RDX) 的催化热分解作用,实验了La0. 8Sr0. 2CoO3-δ粉体对硝胺改性双基推进剂的燃速和压力指数的影响。结果表明: 添加2. 0 % La0. 8Sr0. 2CoO3-δ可使RDX 分解峰温提前, 且分解热增加; 与不加La0. 8Sr0. 2CoO3-δ相比, 在所有的压力下,La0. 8Sr0. 2CoO3-δ的少量添加使推进剂燃速有不同程度的提高,且使推进剂的压强指数降低;与LaCoO3相比,La0. 8Sr0. 2CoO3-δ对硝胺改性双基推进剂的燃烧表现了更好的催化作用。

关键词: 兵器科学与技术, La0. 8Sr0. 2CoO3-δ, 热分解, RDX, 硝胺改性双基推进剂

Abstract:

Perovskite-type La0. 8Sr0. 2CoO3-δ was prepared by a stearic acid gel combustion method in order to investigate the effect of the perovskite oxides on the combustion property of the nitramine modified double-base propellant. The obtained powder is characterized by X-ray powder diffraction (XRD), scanning electron microscopy (SEM),Fourier transform infrared (FT-IR) and X-ray photoelectron spectroscopy (XPS)techniques. The catalytic action of La0. 8Sr0. 2CoO3-δ on the thermal decomposition of hexahydro-1,3,5-trinitro-1,3,5-triazine (RDX) is investigated by TG-DSC technique. The burning rates of nitramine modified double-base propellant at various pressures are studied to evaluate the ballistic property. The experimental results show that La0. 8Sr0. 2CoO3-δ can catalyze the thermal decomposition of RDX, and the heat of decomposition can be increased by 34.7J/g by adding 2.0% (棕) of La0. 8Sr0. 2CoO3-δinto RDX. Compared with basic propellant, the burning rate of propellant modified by La0. 8Sr0. 2CoO3-δ increases at all the pressures. However, the burning rate increases more slowly with the increase of pres-sure, and hence the pressure index of the propellant is reduced. La0. 8Sr0. 2CoO3-δ has the better catalyticaction in comparison with LaCoO3.

Key words: ordnance science and technology, La0. 8Sr0. 2CoO3-δ, thermal decomposition, RDX, nitramine modified double-base propellant

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