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