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Ionic Liquids to Replace HydrazineA method for developing safe, easy-to-handle propellants has been developed based upon ionic liquids (ILs) or their eutectic mixtures. An IL is a binary combination of a typically organic cation and anion, which generally produces an ionic salt with a melting point below 100 deg C. Many ILs have melting points near, or even below, room temperature (room temperature ionic liquids, RTILs). More importantly, a number of ILs have a positive enthalpy of formation. This means the thermal energy released during decomposition reactions makes energetic ILs ideal for use as propellants. In this specific work, to date, a baseline set of energetic ILs has been identified, synthesized, and characterized. Many of the ILs in this set have excellent performance potential in their own right. In all, ten ILs were characterized for their enthalpy of formation, density, melting point, glass transition point (if applicable), and decomposition temperature. Enthalpy of formation was measured using a microcalorimeter designed specifically to test milligram amounts of energetic materials. Of the ten ILs characterized, five offer higher Isp performance than hydrazine, ranging between 10 and 113 seconds higher than the state-of-the-art propellant. To achieve this level of performance, the energetic cations 4- amino-l,2,4-triazolium and 3-amino-1,2,4-triazolium were paired with various anions in the nitrate, dicyanamide, chloride, and 3-nitro-l,2,4-triazole families. Protonation, alkylation, and butylation synthesis routes were used for creation of the different salts.
Document ID
20110012261
Acquisition Source
Armstrong Flight Research Center
Document Type
Other - NASA Tech Brief
Authors
Koelfgen, Syri
(NASA Dryden Flight Research Center Edwards, CA, United States)
Sims, Joe
(Analytical Services, Inc. Huntsville, AL, United States)
Forton, Melissa
(Analytical Services, Inc. Huntsville, AL, United States)
Allan, Barry
(Analytical Services, Inc. Huntsville, AL, United States)
Rogers, Robin
(Alabama Univ. Huntsville, AL, United States)
Shamshina, Julia
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
March 1, 2011
Publication Information
Publication: NASA Tech Briefs, March 2011
Subject Category
Propellants And Fuels
Report/Patent Number
DRC-010-041
Distribution Limits
Public
Copyright
Public Use Permitted.
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