Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant

Released on by Vearl N. Huff
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  • Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant Book Detail

  • Author : Vearl N. Huff
  • Release Date : 1956
  • Publisher :
  • Genre : Charts, diagrams, etc
  • Pages : 58
  • ISBN 13 :
  • File Size : 17,17 MB
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Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant by Vearl N. Huff PDF Summary

Book Description: Data were calculated for equivalence ratios of 1 to 3, chamber pressures of 300 and 600 pounds per square inch absolute, and pressure ratios of 1 to 1500. Parameters included are specific impulse, combustion and exit temperature, molecular weight, characteristic velocity, coefficient of thrust, ratio of nozzle-exit area to throat area, specific heat at constant pressure, isentropic exponent, viscosity, and thermal conductivity. A correlation is given which permits determination of performance for a wide range of chamber pressure.

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