Accession Number : AD0801792
Title : INVESTIGATION AND COMPILATION OF THE THERMODYNAMIC PROPERTIES OF ROCKET EXHAUST PRODUCTS.
Descriptive Note : Quarterly progress rept. no. 3, 1 Jul-30 Sep 66,
Corporate Author : DOW CHEMICAL CO MIDLAND MI THERMAL RESEARCH LAB
Personal Author(s) : Stull, Daniel R. ; Prophet, Harold
Report Date : OCT 1966
Pagination or Media Count : 18
Abstract : A general curve fitting program has been written and modifications made to allow the derivation of heat capacity from enthalpy, and the joining of heat capacity and enthalpy data. Series E of the Propellant Ingredient Tables is being compiled. The low temperature heat capacity of aluminum tribromide has been completed and is reported; the entropy at 298.15 K. is found to be 43.08 gibbs/mole. (Author)
Descriptors : *ROCKET ENGINES), (*EXHAUST GASES, (*THERMODYNAMICS, EXHAUST GASES), ALUMINUM COMPOUNDS, BROMIDES, ENTHALPY, ENTROPY, ROCKET PROPELLANTS, TABLES(DATA), TEMPERATURE.
Subject Categories : Combustion and Ignition
Distribution Statement : APPROVED FOR PUBLIC RELEASE