论文信息 - Thermodynamic Extrapolation of Rocket Performance Parameters

Thermodynamic Extrapolation of Rocket Performance Parameters

[I31 It has been found useful in performance calculations to calculate molecular weight derivatives rather than volume derivatives to indicate changes in composition. From Eq. [I 31 there follows A further discussion of the molecular weight derivatives and a method for their numerical evaluation is given by Gordon et al. (4). With the aid of Bridgman's tables

Sanford Gordon | Frank J. Zeleznik | F. J. Zeleznik | S. Gordon

[1] V. N. Huff,et al. A General Method for Automatic Computation of Equilibrium Compositions and Theoretical Rocket Performance of Propellants , 1959 .

[2] V. N. Huff,et al. Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute , 1953 .

[3] P. W. Bridgman. A condensed collection of thermodynamic formulas , 1925, The Mathematical Gazette.