THERMODYNAMIC PROPERTIES OF PROPELLANT COMBUSTION PRODUCTS

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.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 31, 1965
Accession Number
AD0630634

Entities

People

  • N. D. Potter

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Combustion
  • Combustion Products
  • Effusion
  • Evaporation
  • Heat Energy
  • Heat Of Vaporization
  • High Temperature
  • Mass Spectrometers
  • Mass Spectrometry
  • Materials
  • Measurement
  • Pressure Measurement
  • Spectrometry
  • Thermodynamic Properties
  • Transition Temperature
  • Vapor Pressure
  • Vaporization

Fields of Study

  • Chemistry

Readers

  • Combustion science or combustion engineering.