High Temperature Propellent Reactions: The Determination of the Thermodynamic Properties of their Gaseous Products for use in Heat Engine Calculations

Abstract

AT temperatures below some 2,000°K. the significant end‐products of technically important reactions involving propellents of molecular forms compounded of C, H, O and N atoms are of the following familiar types:

Citation

Osborne, F.E. (1952), "High Temperature Propellent Reactions: The Determination of the Thermodynamic Properties of their Gaseous Products for use in Heat Engine Calculations", Aircraft Engineering and Aerospace Technology, Vol. 24 No. 5, pp. 134-137. https://doi.org/10.1108/eb032157