Journal of Propulsion Technology ›› 2017, Vol. 38 ›› Issue (12): 2851-2856.

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Effects of TKX-50 on Energy of HTPE Propellant and Application Feasibility Analysis

  

  1. Xi’an Modern Chemistry Research Institute,Xi’an 710065,China,Xi’an Modern Chemistry Research Institute,Xi’an 710065,China,Xi’an Modern Chemistry Research Institute,Xi’an 710065,China,Xi’an Modern Chemistry Research Institute,Xi’an 710065,China,Xi’an Modern Chemistry Research Institute,Xi’an 710065,China,Xi’an Modern Chemistry Research Institute,Xi’an 710065,China,Xi’an Modern Chemistry Research Institute,Xi’an 710065,China and Xi’an Modern Chemistry Research Institute,Xi’an 710065,China
  • Published:2021-08-15

TKX-50对HTPE推进剂能量特性的影响及应用可行性

刘运飞,庞维强,谢五喜,张 伟,赵 昱,黄海涛,樊学忠,毕福强   

  1. 西安近代化学研究所,陕西 西安 710065,西安近代化学研究所,陕西 西安 710065,西安近代化学研究所,陕西 西安 710065,西安近代化学研究所,陕西 西安 710065,西安近代化学研究所,陕西 西安 710065,西安近代化学研究所,陕西 西安 710065,西安近代化学研究所,陕西 西安 710065,西安近代化学研究所,陕西 西安 710065
  • 作者简介:刘运飞 ,男,硕士,工程师,研究领域为固体推进剂配方及工艺。
  • 基金资助:
    总装预研项目(40406010102)。

Abstract: In order to explore the feasibility of the application of dihydroxylammonium 5,5’-bistetrazole-1,1’-diolate (TKX-50) in HTPE propellant, the morphology of TKX-50 particles were determined with high grade SEM dynameter. The compatibility of TKX-50 with main compositions of HTPE propellant was investigated by means of DSC and VST, respectively. The effects of different mass fraction of TKX-50 on the energetic characteristics of the propellant were calculated using minimum free energy method. The results show that the morphology of TKX-50 particles are irregular, the particle size distribution is a little not uniform, while the surface of the particles is compact, smooth, and there is no obvious defects. Moreover, there were not obvious interaction between TKX-50 and HTPE, ammonium perchlorate(AP), aluminum (Al) and 2,4-toluene diisocyanate (TDI), while there is a little interactions between TKX-50 and cyclotetramethylene tetranitramine (HMX). With increasing the mass fraction of TKX-50 particles, the specific impulse of HTPE propellant increase significantly. When the mass fraction of TKX-50 is 25%, the maximum theoretical specific impulse is 2685.2N·s·kg-1. And the surface of prepared propellant containing 5% and 15% mass fraction of TKX-50 particles are smooth, and the internal sample is uniform and compact, moreover there is no significant defects, such as reacted pores during the preparation, which indicate that TKX-50 can be applied in the HTPE propellant safely.

Key words: Physical chemistry;TKX-50;Solid propellant;Energy characteristic

摘要: 为探索1,1′—二羟基—5,5′—联四唑二羟胺盐(TKX-50)在端羟基聚醚(HTPE)推进剂中的应用可行性,采用高倍率的扫描电镜观察了TKX-50颗粒的微观形貌,用差示扫描量热法(DSC)和真空安定性试验(VST)法研究了TKX-50与HTPE推进剂主要组分的相容性,并采用最小自由能法计算了TKX-50对HTPE推进剂能量特性的影响规律。结果表明,TKX-50颗粒形貌不规则,且粒度分布不均匀,但颗粒表面致密、光滑,无明显缺陷;TKX-50与粘合剂HTPE、高氯酸铵(AP)、铝粉(Al)和甲苯二异氰酸酯(TDI)之间无明显的相互作用,但与奥克托今(HMX)之间存在一定的相互作用;推进剂配方中添加TKX-50可提高推进剂的能量水平,当TKX-50含量为25%时,推进剂理论比冲达最大值(2685.2N·s·kg-1),且制备的含5%和15%TKX-50的推进剂样品表面光洁,内部均匀且致密,无反应性气孔等异常缺陷,表明TKX-50可安全地应用在HTPE推进剂中。

关键词: 物理化学;TKX-50;固体推进剂;能量性能