高能离子液体的设计

J. Boatz, G. Voth, M. Gordon, S. Hammes‐Schiffer
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引用次数: 10

摘要

美国空军的一项基本需求是发现、开发和部署用于空间和导弹应用的先进化学推进的新型高能材料。推动对新型化学推进剂需求的一些关键因素包括:(a)提高了比冲和密度方面的性能,(b)降低了对冲击、摩擦、冲击和静电放电等外部刺激的敏感性,以及(c)减轻了与目前使用的推进剂相关的环境和毒理学危害(以及由此产生的成本)。一类可能满足这些要求的化合物被称为离子液体(ILs),这是一种熔点异常低的化学盐。il的物理和化学性质使其具有多种用途,最显著的是作为环境无害(“绿色”)溶剂/反应介质,但也可作为催化剂、电解质等。从国防部(DoD)的角度来看,ILs正在被探索作为新的推进剂、炸药和弹药。空军尤其对il感兴趣,因为它有可能取代目前使用的单一推进剂,如肼,它是致癌的,剧毒的,而且性能相对较低。相比之下,许多il具有优越的密度和比脉冲,以及显着降低的敏感性和毒性特性。此外,它们的性质可以通过成分离子的选择来仔细调整。高能离子液体设计挑战项目的总体目标是解决与离子液体作为新型单体推进剂的表征、设计和开发相关的几个关键技术问题和挑战。其中,例如,对il的(in)稳定性的基本理解,短、远程结构的内在性质以及组分离子之间的相互作用,以及对分解和燃烧初始阶段关键步骤的识别。采用了一系列的计算方法,包括应用于单个离子和离子簇的原子的、高水平的量子化学方法,利用极化力场的凝聚态原子分子动力学模拟,以及基于多尺度粗粒化技术的大块离子液体的中尺度模拟。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design of Energetic Ionic Liquids
An essential need of the US Air Force is the discovery, development, and fielding of new, energetic materials for advanced chemical propulsion in space and missile applications. Some of the key factors driving the requirement for new chemical propellants include: (a) improved performance in terms of increased specific impulse and density, (b) reduced sensitivity to external stimuli such as impact, friction, shock, and electrostatic discharge, and (c) mitigation of environmental and toxicological hazards (and the resulting costs) associated with currently used propellants. A class of compounds, which can potentially meet these requirements is known as ionic liquids (ILs), which are chemical salts with unusually low melting points. The physical and chemical properties of ILs render them useful for many purposes, most notably as environmentally benign (“green”) solvents/reaction media but also as catalysts, electrolytes, etc. From a Department of Defense (DoD) perspective, ILs are being explored as new propellants, explosives, and munitions. The Air Force, in particular, is interested in ILs as potential replacements for currently used monopropellants such as hydrazine—which is carcinogenic, highly toxic, and has relatively modest performance characteristics. In contrast, many ILs have superior densities and specific impulses as well as significantly reduced sensitivity and toxicity characteristics. Furthermore, their properties can be carefully tuned via the choice of the component ions. The overall objective of the Design of Energetic Ionic Liquids Challenge Project is to address several key technical issues and challenges associated with the characterization, design, and development of ILs as new monopropellants. Among these, for example, are a fundamental understanding of the (in)stability of ILs, the intrinsic nature of the short- and long-range structure and interactions between the component ions, and identification of the key steps in the initial stages of decomposition and combustion. A hierarchy of computational approaches is employed, including atomistic, high-level quantum chemical methods applied to individual ions and ion clusters, condensed phase atomistic molecular dynamics simulations utilizing polarizable force fields, and mesoscale-level simulations of bulk ionic liquids based upon multiscale coarse graining techniques.
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