Modern engineering for design of liquid-propellant rocket engines /

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Huzel, Dieter K.
Otros Autores: Huang, David H., 1920-, Arbit, Harry
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : American Institute of Aeronautics and Astronautics, 1992.
Colección:Progress in astronautics and aeronautics ; v. 147.
Temas:
Liquid propellant rocket engines > Design and construction.
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Cover
  • Title
  • Copyright
  • Foreword
  • Preface
  • Table of Contents
  • Chapter 1. Introduction to Liquid-Propellant Rocket Engines
  • 1.1 Basic Elements of a Liquid-Propellant Rocket Engine
  • 1.2 Generation of Thrust
  • 1.3 Gas-Flow Processes in the Combustion Chamber and Nozzle
  • The Perfect Gas Law
  • Principle of Conservation of Energy
  • Principle of Conservation of Matter
  • The Isentropic Flow Process
  • Gas Flow Through Liquid-Propellant Rocket Combustion Chambers
  • Gas Flow Through Rocket Nozzles
  • 1.4 Performance Parameters of a Liquid-Propellant Rocket EngineThrust-Chamber Specific Impulse (I[sub(s)])tc
  • Characteristic Velocity c*
  • Thrust Coefficient C[sub(f)]
  • Summary of the Influence of pa, Îæ, γ, R, and (p[sub(c)])ns on Engine Performance
  • Correction Factors and Magnitudes of Engine Performance Parameters
  • 1.5 Liquid Propellants
  • Monopropellants
  • Bipropellants
  • Cryogenic Propellants
  • Storable Liquid Propellants
  • Additives for Liquid Propellants
  • Optimum Mixture Ratio
  • Density Impulse
  • Selection of Liquid Propellants
  • Liquid-Propellant Performance and Physical PropertiesChapter 2. Engine Requirements and Preliminary Design Analyses
  • 2.1 Introduction
  • 2.2 Major Rocket-Engine Design Parameters
  • Thrust Level
  • Performance
  • Duration
  • Mixture Ratio
  • Weight
  • Envelope (Size)
  • Reliability
  • Cost
  • Availability (Scheduling)
  • 2.3 Mission Requirements
  • Typical Mission Goals
  • Typical Vehicle Requirement Optimization
  • 2.4 Engine Preliminary Design
  • Engine System and Component Concepts
  • Preliminary Design Optimization
  • 2.5 Design Philosophy
  • The Importance of Design QualitySystems Analysis and Design Layout
  • Stress Analysis
  • Selection of Materials
  • Chapter 3. Introduction to Sample Calculations
  • 3.1 Approach
  • 3.2 A-1 Stage Engine
  • General Engine-System Description
  • System Operation
  • 3.3 A-2 Stage Engine
  • General Engine-System Description
  • System Operation
  • Starting Sequence
  • Cutoff Sequence
  • 3.4 A-3 Stage Engine
  • General Engine-System Description
  • System Operation
  • 3.5 A-4 Stage Engine
  • General Engine System Description
  • System Operation
  • Chapter 4. Design of Thrust Chambers and Other Combustion Devices4.1 Basic Thrust-Chamber Elements
  • 4.2 Thrust-Chamber Performance Parameters
  • Specific Impulse I[sub(s)] (s)
  • Characteristic Velocity c* (ft/s)
  • Thrust Coefficient C[sub(f)] (Dimensionless)
  • Performance Calculation
  • 4.3 Thrust-Chamber Configuration Layout
  • Combustion-Chamber Volume
  • Combustion-Chamber Shape
  • Nozzle Expansion Area Ratio
  • Nozzle Shape
  • Clustered-Nozzle Concepts
  • Alternate Solution
  • 4.4 Thrust-Chamber Cooling
  • Cooling Techniques and Selection

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