4.4 Article

Graphene Oxide/Ammonium Perchlorate Composite Material for Use in Solid Propellants

期刊

JOURNAL OF PROPULSION AND POWER
卷 32, 期 3, 页码 682-686

出版社

AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.B35815

关键词

-

资金

  1. U.S. Air Force Office of Scientific Research Multidisciplinary University Research Initiative (MURI) [FA9550-13-1-0004]

向作者/读者索取更多资源

An energetic composite material based on graphene oxide and ammonium perchlorate was prepared using a recrystallization method involving acetone and ethyl acetate as the solvent and antisolvent, respectively. This method resulted in the production of small crystals, where the graphene oxide wraps around the ammonium perchlorate particle to form a composite particle. The resulting composite material is found to enhance the thermal decomposition of ammonium perchlorate over just physically mixing. Furthermore, using this material, bimodal ammonium perchlorate/hydroxyl-terminated polybutadiene solid propellants were prepared. The combustion behavior of the propellants were investigated, and the graphene-oxide-based solid propellant resulted in a 15% increase in the burning rate at a pressure of 80 atm over the baseline material.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.4
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据