研究某些因素对带有端链羧基的丙烯腈丁二烯橡胶载能材料高燃烧率的影响

Duc-Long Nguyen, Van Hung Nguyen, Huu-Thanh Tran, Van Diep Doan, Van Hung Hoang
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引用次数: 0

摘要

与其他载能材料相比,异质载能材料具有突出的优势,因此,研究和开发这类材料以制造飞行物推进器是军事科学和航天领域的必然趋势。本文介绍了以丙烯腈-丁二烯橡胶 CKH-10KTP 和高氯酸铵(AP)为基础的异质载能材料的技术性能和燃烧速率受多种因素影响的研究成果。研究结果表明,以 CKH-10KTP 和超细 AP(比表面积为 2.61÷3.85 m2/g)为基础的异质载能材料,使用二茂铁衍生物燃烧催化剂,其燃烧规律取决于压力。研究还确定了燃烧催化剂-增塑剂的最佳含量为 3.5%÷3.8%。研究成果为优化确定载能材料的放射性、能量参数提供了坚实的科学依据,补充了飞机发动机设计中的国家数据来源,满足了新形势下的要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Study on the influence of some factors on the high burning rate of energy-carrying materials based on acrylonitrile butadiene rubber with end-chain carboxyl group
Heterogeneous energy-carrying materials possess outstanding advantages compared to other energy-carrying materials, therefore, research and development of this type of material to create propulsion for flying objects is an inevitable trend in the field of military science and space. This paper presents the results of research on the influence of a number of factors on the technological properties and combustion rate of heterogeneous energy-carrying materials based on acrylonitrile butadiene rubber CKH-10KTP and ammonium perchlorate (AP).The research results show that the combustion law depends on the pressure of heterogeneous energy-carrying materials based on CKH-10KTP and ultra-fine AP (specific surface area 2.61÷3.85 m2/g), using a combustion catalyst ferrocene derivative. The study also determined the optimal content of combustion catalyst - plasticiser to be 3.5÷3.8%. The research results are a solid scientific basis for optimally determining the parameters of radioactivity, energy of energy-carrying materials, supplementing the national data source in the design of aircraft engines, meeting requirements in the new context.
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