Accession Number : AD0625598

Title :   THERMODYNAMIC PROPERTIES OF ROCKET EXHAUST PRODUCTS.

Descriptive Note : Quarterly rept. no. 1, 1 Aug-31 Oct 65,

Corporate Author : ROCKET POWER INC PASADENA CALIF RESEARCH LABS

Personal Author(s) : Greenbaum,M. A. ; Yates,R. E. ; Frisch,M. A. ; Ko,H. C. ; Farber,M.

Report Date : 31 OCT 1965

Pagination or Media Count : 25

Abstract : Experiments are to be performed on thermodynamic and physical properties of some of the compounds of light metals likely to be formed by the combustion of solid or hybrid propellants and their additives at temperatures of 2000 to 5000K. The thermodynamic properties are to be determined for gaseous BeOH, BOH, and AlCl2, and the entropy of Be(OH)2 is to be determined. Apparatus was assembled and constructed for these experiments.

Descriptors :   (*ROCKET PROPELLANTS, COMBUSTION PRODUCTS), (*EXHAUST GASES, THERMOCHEMISTRY), (*THERMODYNAMICS, ROCKET PROPELLANTS), (*BORON COMPOUNDS, HYDROXIDES), (*BERYLLIUM COMPOUNDS, HYDROXIDES), (*ALUMINUM COMPOUNDS, HYDROXIDES), HYBRID ROCKET ENGINES, SOLID PROPELLANT ROCKET ENGINES, ENTROPY, ADDITIVES, HIGH TEMPERATURE

Subject Categories : Combustion and Ignition
      Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE