CHEMICAL CORROSION OF ROCKET LINER MATERIALS AND PROPELLANT PERFORMANCE STUDIES THERMODYNAMIC PROPERTIES OF HEAVY METAL SPECIES. VOLUME 2

Abstract

As part of a study of the chemical corrosion of rocket liner materials, many computations were made of the chemical equilibria between rocket liner materials and corrosive gaseous or condensed materials. As a convenience to readers, who may be interested in the thermodynamic properties for their own sake, all the properties developed during the contract period are collected in this single volume. For each species considered, the literature was searched to uncover whatever data were available; these were then evaluated in an attempt to use the most reliable data. For most species direct experimental results were lacking in some particular, and judicious estimates of the missing data were required.

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Document Details

Document Type
Technical Report
Publication Date
Dec 15, 1963
Accession Number
AD0425887

Entities

People

  • R. W. Sprague

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Atoms
  • Enthalpy
  • Equations
  • Ground State
  • Heat Capacity
  • Heat Energy
  • Heat Of Formation
  • Heat Of Fusion
  • Materials
  • Melting Point
  • Metals
  • Moment Of Inertia
  • Phase Diagrams
  • Specific Heat
  • Thermodynamic Properties
  • Tungsten
  • Tungsten Compounds

Readers

  • Combustion science or combustion engineering.
  • Environmental Engineering.
  • Theoretical Analysis.