Performance Evaluation of Liquid Fuel 2-Dimethyl Amino Ethyl Azide (DMAZ) with Liquid Oxidizers

REFERENCES

• Schmidt , E. W. 2001 . Hydrazine and Its Derivatives . New York : John Wiley & Sons .
   Google Scholar
• Sutton , G. P. and P. Biblarz . 2010 . Rocket Propulsion Elements . New York : John Wiley & Sons .
   Google Scholar
• Sengupta , D. and S. Raman . 2007 . Theoretical investigation of some high-performance novel amine azide propellants . Propellants, Explosives, Pyrotechnics , 32 : 338 – 347 .
   Web of Science ®Google Scholar
• Agrawal , J. P. 2010 . High Energy Materials: Propellants, Explosives and Pyrotechnics . Weinheim , Germany : Wiley-VCH .
   Google Scholar
• Keshavarz , M. H. 2006 . A simple procedure for assessing the performance of liquid propellants . High Temperature–High Pressure , 35/36 : 587 – 592 .
   Google Scholar
• Durgapal , U. C. , P. K. Dutta , G. C. Pant , M. B. Ingalgaonkar , V. Y. Oka , and B. B. Umap . 1987 . Studies on hypergolicity of several liquid fuels with fuming nitric acids as oxidizers . Propellants, Explosives, Pyrotechnics , 12 : 149 – 153 .
   Google Scholar
• Wright , A. C. 1977 . USAF Propellant Handbooks. Nitric Acid/Nitrogen Tetroxide Oxidizers . Volume II . Cloudcroft , NM : Ft. Belvoir Defense Technical Information Center . AD-A03674 .
   Google Scholar
• Kokan , T. S. , J. R. Olds , J. M. Seitzman , and P. J. Ludovice . 2009 . Characterizing high-energy-density propellants for space propulsion applications . Acta Astronautica , 65 : 967 – 986 .
   Web of Science ®Google Scholar
• Reddy , G. , J. Song , M. S. Mecchi , and M. S. Johnson . 2010 . Genotoxicity assessment of two hypergolic energetic propellant compounds . Mutation Research/Genetic Toxicology and Environmental Mutagenesis , 700 : 26 – 31 .
   PubMed Web of Science ®Google Scholar
• Schiemenz , P. and H. Engelhard . 1959 . Trimethoxyphenyl derivatives. I. synthesis of amines via mixed anhydrides . Chemische Berichte , 92 : 857 – 862 .
   Google Scholar
• Sanford , G. and B. J. McBride . 1994 . Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications. I. Analysis . Vol. 1331 . NASA Reference Publication , Washington , DC .
   Google Scholar
• Wang , S. Q. and S. T. Thynell . 2012 . An experimental study on the hypergolic interaction between monomethylhydrazine and nitric acid . Combustion and Flame , 159 : 438 – 447 .
   Web of Science ®Google Scholar
• Edwards , T. 2003 . Liquid fuels and propellants for aerospace propulsion: 1903–2003 . Journal of Propulsion and Power , 19 : 1089 – 1107 .
   Web of Science ®Google Scholar
• Liu , W. G. , S. Dasgupta , S. V. Zybin , and W. A. Goddard . 2011 . First principles study of the ignition mechanism for hypergolic bipropellants: N,N,N′,N′-tetramethyleethylene diamine (TMEDA) and N,N,N′,N′-tetramethylmethylene diamine (TMMDA) with nitric acid . Journal of Physical Chemistry. A , 115 : 5221 – 5229 .
   PubMed Web of Science ®Google Scholar
• Pourpoint , T. L. and W. E. Anderson . 2009 . Hypergolic reaction mechanisms of catalytically promoted fuels with rocket grade hydrogen peroxide . Combustion Science and Technology , 179 : 2107 – 2133 .
   Web of Science ®Google Scholar
• Hallit , R. E. A. and G. Bauerle . 2005 . Hypergolic Azide Fuels with Hydrogen Peroxide . U.S. Patent #6949152 B2.
   Google Scholar
• Schneider , S. , T. Hawkins , Y. Ahmed , S. Deplazes , and J. Mills . 2012 . Ionic liquid fuels for chemical propulsion. In Ionic Liquids: Science and Applications, pp. 1–25. Washington, DC: American Chemical Society.
   Google Scholar
• Color versions of one or more of the figures in the article can be found online at www.tandfonline.com/uegm.
   Google Scholar