One Method of Determining the Criterion of Operational Stability of a Liquid-Propellant Rocket Engine

Abstract

Presented is a method of determining the criterion of operational stability of a liquid-propellant rocket engine.

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Document Details

Document Type
Technical Report
Publication Date
Aug 16, 1963
Accession Number
AD0420602

Entities

People

  • G. I. Zamuruyev

Organizations

  • Air Force Systems Command

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Chambers
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Differential Equations
  • Energy
  • Engines
  • Equations
  • Flow
  • Fluid Flow
  • Kinetic Energy
  • Liquid Propellant Rocket Engines
  • Liquid Propellants
  • Oscillation
  • Propellants
  • Rocket Engines
  • Rockets

Fields of Study

  • Physics