Burning characteristics of ammonium nitrate propellant containing fine ammonium perchlorate – influence of porosity of ammonium perchlorate**

Author:

Tsuchiya Hironori1,Togashi Ryoto1,Kohga Makoto1ORCID

Affiliation:

1. Department of Applied Chemistry National Defence Academy Hashirimizu 1-10-20 Yokosuka Kanagawa 239-8686 Japan

Abstract

AbstractFine porous ammonium perchlorate (PAP) has small holes in its crust, and the voids in the particles are connected to the outside. The porosity of PAP results in fine bubble contamination in a propellant because the voids in PAP cannot be completely charged with a binder. Fine bubble contamination can improve the burning rate characteristics of an ammonium perchlorate (AP) propellant. The influence of the porosity of PAP on the burning characteristics of an ammonium nitrate (AN)/AP propellant and the effect of Fe2O3 as a catalyst on them were investigated in this study. The void fraction of the propellant increased with increasing mass ratio between AP and all oxidizers (ξ) and ranged from 1.3 % to 3.2 %. The porosity of PAP increased the burning rate of AN/AP propellants. This effect increased with decreasing pressure and was independent of ξ. However, porosity had minimal influence on the burning rate of AN/AP propellants with Fe2O3. The effect of the catalyst on the increase in the burning rate due to the porosity of PAP was influenced by pressure and ξ. The effect on the AN/AP propellant was greatest when ξ was in the 0.5–0.6 range.

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Reference38 articles.

1. Sutton G. P. (1992) Rocket Propulsion Element Sixth Edition John Wily & Sons Inc. New York p. 420.

2. Ammonium nitrate: a promising rocket propellant oxidizer

3. Combustion Mechanism of Ammonium-Nitrate-Based Propellants

4. Ammonium Nitrate as an Eco–Friendly Oxidizer for Composite Solid Propellants: Promises and Challenges

5. The Effect of Ammonium Nitrate, Coarse/Fine Ammonium Nitrate Ratio, Plasticizer, Bonding Agent, and Fe2O3 Content on Ballistic and Mechanical Properties of Hydroxyl Terminated Polybutadiene Based Composite Propellants Containing 20 % AP;Nihal Tüzün F.;J. ASTM Int.,2005

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