Liquid rocket engine thrust chamber : parametrical modeling /

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This book presents an innovative parametric model applicable to the project of some elements of the liquid rocket thrust chamber with the level of detail and accuracy appropriate to the preliminary design phase. It addresses the operating characteristics and dimensioning of some thrust chamber eleme...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Rezende, Rene Nardi
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Warrendale, Pa. (400 Commonwealth Dr., Warrendale PA USA) : Society of Automotive Engineers, 2018.
Colección:Society of Automotive Engineers. Electronic publications
Temas:
Space vehicles > Propulsion systems.
Rockets (Aeronautics)
Véhicules spatiaux > Propulsion.
Fusées (Aéronautique)
TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics.
Space vehicles > Propulsion systems
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Chapter 1. Introduction
  • Chapter 2. Fundamentals of rcket populsion
  • Chapter 3. Methodology
  • Chapter 4. Thrust chamber performance assessment
  • Chapter 5. Nozzle dimensioning
  • Chapter 6. Combustion chamber dimensioning
  • Chapter 7. Nozzle configuration
  • Chapter 8. Complementing the performance calculation
  • Chapter 9. The cold section
  • Chapter 10. The simplex swirl injector
  • Chapter 11. The Pintle injector
  • Appendix.

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