INVESTIGATION OF NONEQUILIBRIUM PHENOMENA IN ROCKET NOZZLES.

Abstract

Progress in the program for the Investigation of Nonequilibrium Phenomena in Rocket Nozzles for the period 1 July to 31 December 1958 is described. Theoretical calculations were carried out for the hydrazine-fluorine propellant system to obtain design data for the kinetics shock tube facility. These studies include calculation of thermodynamic properties for hydrazine-fluorine systems and shock calculations. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 31, 1958
Accession Number
AD0607110

Entities

People

  • J. G. Logan

Organizations

  • TRW Inc.

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Fluorine
  • Gas Turbine Nozzles
  • Hydrazines
  • Kinetics
  • Nozzles
  • Propellants
  • Rocket Nozzles
  • Rockets
  • Shock Tubes
  • Thermodynamic Properties
  • Tubes

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Technical Research and Report Writing.