Effects of aluminum composites on the regression rates of solid fuels

Author:

Paravan C.,Penazzo S.,Dossi S.,Stocco M.,DeLuca L.T.,Galfetti L.

Abstract

Innovative, mechanically activated Al–polytetrafluoroethylene (PTFE) composites and ammonium perchlorate (AP) coated nano-sized aluminum (C-ALEX) were produced, characterized, and tested as solid fuel additives. The ballistics of fuel formulations based on hydroxylterminated polybutadiene (HTPB) was investigated in a microburner by a time-resolved technique for regression rate (rf) data reduction. Both Al-composites show promising results in terms of rf and mass burning rate enhancement. In particular, the C-ALEX showed a percent rf increase over the baseline (HTPB) of 27% at an oxidizer mass flux of 350 kg/(m2s), without requiring dedicated dispersion procedures. This performance enhancement was nearly constant over the whole investigated range.

Publisher

EDP Sciences

Reference50 articles.

1. Altman D., and Holzman A.. 2008. Overview and history of hybrid rocket propulsion. Fundamentals of hybrid rocket combustion and propulsion. Eds. Chiaverini M. J. and Kuo K. K.. AIAA progress in astronautics and aeronautics ser. Vol. 218. Ch. 1. P. 1–36.

2. Chiaverini M. J. 2007. Review of solid fuel regression rate behavior in classical and non-classical hybrid rocket motors. Fundamentals of hybrid rocket combustion and propulsion. Eds. Chiaverini M. J. and Kuo K. K.. AIAA progress in astronautics and aeronautics ser. Vol. 218. Ch. 2. P. 37–125.

3. Marxman G. A., and Gilbert M.. 1963. Turbulent boundary layer combustion in the hybrid rocket. 9th Symposium (International) on Combustion. New York, NY: Academic Press, Inc. 371–383.

4. Marxman G. A. 1967. Boundary layer combustion in propulsion. 11th Symposium (International) on Combustion Proceedings. Pittsburg, PA: The Combustion Institute. 269–289.

5. Marxman G. A., and Wooldridge C. E.. 1968. Research on the combustion mechanism of hybrid rockets. Advances in tactical rocket propulsion: AGARD Conference Proceedings. Ed. Penner S. S.. 1:421–477.

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. The Effects of Fluorine-Containing Additives in Composite Propellants with Boron and Aluminum Dodecaboride on the Characteristics of Their Combustion;Journal of Engineering Physics and Thermophysics;2022-12

2. Enhancing Micrometric Aluminum Reactivity by Mechanical Activation;Innovative Energetic Materials: Properties, Combustion Performance and Application;2020

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3