Advances in Chemical Propulsion by Roy G.D. (ed.)

By Roy G.D. (ed.)

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The contents of the flask were cooled to −60 ◦ C and the DMSO solution was added dropwise in ca. 5 min. Stirring was continued at −60 ◦ C for 10 min followed by addition of the diol solution in ca. 5 min. The reaction mixture was stirred for 15 min and TEA (or DIPEA: 24 mmol) was added in ca. 5 min with stirring at −60 ◦ C. The cooling bath was removed and water (30 ml) was added at room temperature. The aqueous layer is reextracted with dichloromethane, organic layers are combined, washed with saturated sodium chloride solution (100 ml), and dried with anhydrous magnesium sulfate.

In conclusion, although quantum improvements have not been achieved, there has been phenomenal growth in understanding the various fundamental mechanisms in combustion devices, and applying them scientifically and more effectively for designing practical propulsion systems. Some of the major accomplishments in the various aspects of combustion for propulsion engines have been elucidated. Future opportunities in combustion research call for multidisciplinary programs with a balanced emphasis on analysis, computations, diagnostics, and experimentation.

Strykowski, P. , A. Krothapalli, and S. Jendoubi. 1996. The effect of counterflow on the development of compressible shear layers. J. Fluid Mechanics 308:63–96. 7. Gutmark, E. , K. S. Schadow, and K. H. Yu. 1997. Mixing enhancement in supersonic free shear flows. Annual Reviews Fluid Mechanics 27:375–417. 8. Baer, D. , M. E. Newfield, N. Gopaul, and R. K. Hanson. 1994. Multiplexed diode laser sensor system for simultaneous H2 O, O2 and temperature measurements. Optic Letters 19(22):1900–2. 9. Strykowski, P.

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