Combustion instabilities in liquid rocket engines testing and development practices in Russia /

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Detalles Bibliográficos
Autor Principal: Dranovsky, Mark L.
Autor Corporativo: ebrary, Inc
Outros autores: Yang, Vigor, Culick, F. (Fred), 1933-, Talley, Douglas G.
Formato: Electrónico eBook
Idioma:inglés
Publicado: Reston, Va. : American Institute of Aeronautics and Astronautics, c2007.
Series:Progress in astronautics and aeronautics.
Subjects:
Acceso en liña:An electronic book accessible through the World Wide Web; click to view
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Table of Contents:
  • Introduction
  • Terms and definitions
  • Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level
  • Uncertainty in conversion of propellant to combustion products
  • Studies of operating process stability at various stages of combustor development
  • Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators
  • Acoustic study of combustion chamber stability characteristics
  • Determination of stability of oscillations from natural disturbances
  • Evaluation of LRE process stability by use of artificial pressure disturbances
  • Model firing tests for selection of injector head elements
  • Estimation of operating process stability from pressure oscillation decrements
  • Test results for pulsing liquid-liquid chambers
  • Stability of gas-liquid combustion chambers
  • Gas-liquid combustion-chamber tests for stability to hard excitation
  • Injector head for RD-170 engine combustion chamber
  • Stability characteristics of engines with adjustable injectors
  • Control of stability in production of the proton engine.