Accession Number : AD0754329

Title :   Thermodynamic and Thermophysical Properties of Combustion Products. Methods of Calculation,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Alemasov,V. E. ; Dregalin,A. F.

Report Date : 29 SEP 1972

Pagination or Media Count : 644

Abstract : The handbook contains information about the combustion products of high-energy propellants. Two- and three-component propellant compositions are examined. Among the active oxidizers, oxygen and fluorine, mixtures of them, and also compounds rich in oxygen and fluorine are examined. Among the high-energy fuels a preferential place is occupied by compounds rich in hydrogen, and also metalliferous fuels. Information is also given about the combustion products of some fuels with air and the decomposition products of some compounds used as monopropellants. Primarily the report discusses the thermodynamics used in understanding the combustion and combustion products.

Descriptors :   (*ROCKET PROPELLANTS, *COMBUSTION), (*THERMODYNAMICS, ROCKET PROPELLANTS), LIQUID ROCKET PROPELLANTS, LIQUID ROCKET OXIDIZERS, COMBUSTION PRODUCTS, MATHEMATICAL ANALYSIS, ENTHALPY, EQUATIONS OF STATE, CHEMICAL EQUILIBRIUM, COMPUTER PROGRAMMING, GAS FLOW, HALOGENATED HYDROCARBONS, OXIDES, METALS, USSR

Subject Categories : Physical Chemistry
      Combustion and Ignition
      Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE