Theoretical rocket performance of JP-4 fuel with mixtures of liquid ozone and fluorine

Huff, Vearl N Gordon, Sanford
naca-rm-e56k14
January 28, 1957


Data were estimated by means of a heat correction equation using data for JP-4 fuel with mixtures of oxygen and flourine. The estimated data were checked for several cases by direct calculations. The difference in specific impulse between the estimated and directly calculated values was from 0.2 to 0.8 pound-second per pound. The maximum value of specific impulse was 334.9 pound-seconds per pound for a combustion-chamber pressure of 600 pounds per square inch absolute and an exit pressure of 1 atmosphere.

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