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Experimental solid and liquid propellant rocket development in Universiti Teknologi Malaysia: 1992-2011

机译:马来西亚Teknologi大学实验性固体和液体推进剂火箭的研制:1992-2011年

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摘要

This paper reports on the research and development activities related to the experimental solid and liquid propellant rocket in Universiti Teknologi Malaysia (UTM) from year 1992 to 2011. A total of 41 closed access academic theses and project papers from UTM library archive were exclusively selected for this review work. Some of these theses and papers originally written in Malay language were translated into English language in this paper for better understanding of the research community. This paper gives a historical insight on the apparatus and methodology designed for educational research activities related to rocket propulsion in UTM. With the available resources within UTM, a few chemical propellant using Ammonium Perchlorate, Potassium Nitrate and hydrogen peroxide as oxidizer were tested in UTM propulsion lab. Besides discussing the rocket fuel components, composite rocket body, ceramic nozzle and alternative binder using natural rubber also covered in this review work. Significant experimental results and numerical findings achieved by UTM researchers were included in this paper.
机译:本文报道了1992年至2011年马来西亚Teknologi大学(UTM)与实验性固体和液体推进剂火箭有关的研究和开发活动。共有41篇来自UTM图书馆档案馆的封闭存取学术论文和项目论文被专门选作这项审查工作。这些最初以马来语撰写的论文和论文中,有一些已被翻译成英文,以更好地了解研究界。本文对用于与UTM火箭推进有关的教育研究活动设计的装置和方法提供了历史性见解。利用UTM内的可用资源,在UTM推进实验室测试了一些使用高氯酸铵,硝酸钾和过氧化氢作为氧化剂的化学推进剂。除了讨论火箭的燃料成分外,本综述工作还涵盖了复合火箭主体,陶瓷喷嘴和使用天然橡胶的替代粘合剂。本文包含了UTM研究人员获得的重要实验结果和数值发现。

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