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):

Report Date:

1966-10-01

Pagination or Media Count:

18.0

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 gibbsmole. Author

Subject Categories:

  • Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE