Progress in the program for the Investigation of Nonequilibrium Phenomena in Rocket Nozzles for the period 1 July to 31 December 1958 is described. Theoretical calculations were carried out for the hydrazine-fluorine propellant system to obtain design data for the kinetics shock tube facility. These studies include calculation of thermodynamic properties for hydrazine-fluorine systems and shock calculations. Author
Semiannual rept. for 1 Jul-31 Dec 58,
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