Thermodynamic Extrapolation of Rocket Performance Parameters SANFORD GORDON '
نویسندگان
چکیده
First and second partial derivatives of some thermodynamically defined rocket performance parameters are presented. Theae derivatives are useful for the extrapolation and interpolation of thermodynamic performance calculations for changes in combustion pressure, combustion enthalpy, pressure ratio, and area ratio. The accuracy of the extrapolation or interpolation is indicated for a typical propellant combination.
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