Accession Number:

AD0630634

Title:

THERMODYNAMIC PROPERTIES OF PROPELLANT COMBUSTION PRODUCTS

Descriptive Note:

Quarterly letter rept. no. 2, 1 Sep-31 Dec 1965

Corporate Author:

PHILCO NEWPORT BEACH CA AERONUTRONIC DIV

Personal Author(s):

Report Date:

1965-12-31

Pagination or Media Count:

8.0

Abstract:

The objective of this program is to provide thermodynamic data for species which are potentially important combustion products of advanced chemical rockets and for related species. Enthalpy and entropy data are obtained from equilibrium measurements made by torsion-free evaporation and torsion-effusion techniques and by high temperature mass spectrometry.

Subject Categories:

  • Atomic and Molecular Physics and Spectroscopy
  • Combustion and Ignition
  • Rocket Propellants
  • Inorganic Chemistry

Distribution Statement:

APPROVED FOR PUBLIC RELEASE