Thermodynamic Extrapolation of Rocket Performance Parameters

SANFORD GORDON; FRANK J. ZELEZNIK

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Article . 1962 . Peer-reviewed

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https://dx.doi.org/10.2514/8.6...

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Thermodynamic Extrapolation of Rocket Performance Parameters

descriptionPublicationkeyboard_double_arrow_right Article 01 Aug 1962 English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:ARS Journal, volume 32, pages 1,195-1,202 (eissn: 1936-9972,

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Authors: SANFORD GORDON; FRANK J. ZELEZNIK;

doi: 10.2514/8.6243

Thermodynamic Extrapolation of Rocket Performance Parameters

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Abstract

[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

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National Aeronautics and Space Administration
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