INVESTIGATION AND COMPILATION OF THE THERMODYNAMIC PROPERTIES OF ROCKET EXHAUST PRODUCTS.
Quarterly progress rept. no. 3, 1 Jul-30 Sep 66,
DOW CHEMICAL CO MIDLAND MI THERMAL RESEARCH LAB
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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 gibbsmole. Author
- Combustion and Ignition