• DocumentCode
    2421902
  • Title

    Design of Energetic Ionic Liquids

  • Author

    Boatz, Jerry A. ; Gordon, Mark S. ; Voth, Gregory A. ; Hammes-Schiffer, Sharon

  • Author_Institution
    Space & Missile Propulsion Div., Air Force Res. Lab., Edwards AFB, CA
  • fYear
    2008
  • fDate
    14-17 July 2008
  • Firstpage
    196
  • Lastpage
    200
  • Abstract
    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 (ldquogreenrdquo) 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 stage- - s 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.
  • Keywords
    explosives; missiles; product design; propellants; quantum chemistry; US air force; atomistic molecular dynamics; chemical propellants; chemical propulsion; combustion; decomposition; energetic ionic liquids; energetic materials; monopropellants development; multiscale coarse graining techniques; project design; quantum chemical methods; toxicological hazards; Chemical hazards; Computational modeling; Electric shock; Friction; Liquids; Missiles; Propellants; Propulsion; Quantum computing; Toxic chemicals;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    DoD HPCMP Users Group Conference, 2008. DOD HPCMP UGC
  • Conference_Location
    Seattle, WA
  • Print_ISBN
    978-1-4244-3323-0
  • Type

    conf

  • DOI
    10.1109/DoD.HPCMP.UGC.2008.57
  • Filename
    4755865