THERMODYNAMIC PROPERTIES OF PROPELLANT COMBUSTION PRODUCTS
Abstract
The objective of the program is to provide thermodynamic data for species which are potentially important combustion products of advanced chemical rockets and for species which are related to these. Enthalpy and entropy data are obtained from equilibrium measurements made by torsion-free evaporation and torsion-effusion techniques and by high temperature mass spectrometry.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 31, 1965
- Accession Number
- AD0625044
Entities
People
- N. D. Potter