Rocket propulsion elements

Rocket propulsion elements

Detalles Bibliográficos
Otros Autores: Biblarz, Oscar, author (author)
Formato: Libro electrónico
Idioma:Inglés
Publicado: Hoboken, N.J.: John Wiley & Sons c2017.
Hoboken, New Jersey : 2017.
Edición:Ninth edition
Materias:
Rocket engines.
Ver en Biblioteca Universitat Ramon Llull:https://discovery.url.edu/permalink/34CSUC_URL/1im36ta/alma991009849112006719
Tabla de Contenidos:
  • Cover
  • Title Page
  • Copyright
  • Contents
  • Preface
  • Chapter 1: Classification
  • 1.1. Duct Jet Propulsion
  • 1.2. Rocket Propulsion
  • Chemical Rocket Propulsion
  • Combinations of Ducted Jet Engines and Rocket Engines
  • Nuclear Rocket Engines
  • Electric Rocket Propulsion
  • Other Rocket Propulsion Concepts
  • International Rocket Propulsion Effort
  • 1.3. Applications of Rocket Propulsion
  • Space Launch Vehicles
  • Spacecraft
  • Military and Other Applications
  • References
  • Chapter 2: Definitions and Fundamentals
  • 2.1. Definitions
  • 2.2. Thrust
  • 2.3. Exhaust Velocity
  • 2.4. Energy and Efficiencies
  • 2.5. Multiple Propulsion Systems
  • 2.6. Typical Performance Values
  • 2.7. Variable Thrust
  • Symbols
  • Greek Letters
  • Problems
  • References
  • Chapter 3: Nozzle Theory and Thermodynamic Relations
  • 3.1. Ideal Rocket Propulsion Systems
  • 3.2. Summary of Thermodynamic Relations
  • 3.3. Isentropic Flow through Nozzles
  • Velocity
  • Nozzle Flow and Throat Condition
  • Thrust and Thrust Coefficient
  • Characteristic Velocity and Specific Impulse
  • Under- and Overexpanded Nozzles
  • Influence of Chamber Geometry
  • 3.4. Nozzle Configurations
  • Cone- and Bell-Shaped Nozzles
  • 3.5. Real Nozzles
  • Boundary Layers
  • Multiphase Flow
  • Other Phenomena and Losses
  • Performance Correction Factors
  • Four Performance Parameters
  • 3.6. Nozzle Alignment
  • Symbols
  • Greek Letters
  • Subscripts
  • Problems
  • References
  • Chapter 4: Flight Performance
  • 4.1. Gravity-Free Drag-Free Space Flight
  • 4.2. Forces Acting on a Vehicle in the Atmosphere
  • 4.3. Basic Relations of Motion
  • 4.4. Space Flight
  • Elliptical Orbits
  • Deep Space
  • Perturbations
  • Mission Velocity
  • 4.5. Space Flight Maneuvers
  • Reaction Control System
  • 4.6. Effect of Propulsion System on Vehicle Performance
  • 4.7. Flight Vehicles.
  • Multistage Vehicles
  • Stage Separation
  • Launch Vehicles
  • 4.8. Military Missiles
  • 4.9. Flight Stability
  • Symbols
  • Greek Letters
  • Subscripts
  • Problems
  • References
  • Chapter 5: Chemical Rocket Propellant Performance Analysis
  • 5.1. Background and Fundamentals
  • 5.2. Analysis of Chamber or Motor Case Conditions
  • 5.3. Analysis of Nozzle Expansion Processes
  • 5.4. Computer-Assisted Analysis
  • 5.5. Results of Thermochemical Calculations
  • Symbols
  • Greek Letters
  • Subscripts
  • Problems
  • References
  • Chapter 6: Liquid Propellant Rocket Engine Fundamentals
  • 6.1. Types of Propellants
  • 6.2. Propellant Tanks
  • 6.3. Propellant Feed Systems
  • Local Pressures and Flows
  • 6.4. Gas Pressure Feed Systems
  • 6.5. Tank Pressurization
  • Factors Influencing the Required Mass of Pressurizing Gas
  • Simplified Analysis for the Mass of Pressurizing Gas
  • 6.6. Turbopump Feed Systems and Engine Cycles
  • Engine Cycles
  • 6.7. Rocket Engines for Maneuvering, Orbit Adjustments, or Attitude Control
  • 6.8. Engine Families
  • 6.9. Valves and Pipelines
  • 6.10. Engine Support Structure
  • Symbols
  • Subscripts
  • Problems
  • References
  • Chapter 7: Liquid Propellants
  • 7.1. Propellant Properties
  • Economic Factors
  • Performance of Propellants
  • Common Physical Hazards
  • Desirable Physical Properties
  • Ignition, Combustion, and Flame Properties
  • Property Variations and Specifications
  • Additives
  • 7.2. Liquid Oxidizers
  • Liquid Oxygen (O2) (LOX)
  • Hydrogen Peroxide (H2O2)
  • Nitric Acid (HNO3)
  • Nitrogen Tetroxide (N2O4) (NTO)
  • Nitrous Oxide (N2O)
  • Oxidizer Cleaning Process
  • 7.3. Liquid Fuels
  • Hydrocarbon Fuels
  • Liquid Hydrogen
  • Hydrazine (N2H4)
  • Unsymmetrical Dimethylhydrazine [(CH3)2NNH2]
  • Monomethylhydrazine (CH3NHNH2)
  • 7.4. Liquid Monopropellants
  • Hydrazine as a Monopropellant
  • 7.5. Gaseous Propellants.
  • 7.6. Safety and Environmental Concerns
  • Symbols
  • Greek Letters
  • Problems
  • References
  • Chapter 8: Thrust Chambers
  • 8.1. Injectors
  • Injector Flow Characteristics
  • Factors Influencing Injector Behavior
  • 8.2. Combustion Chamber and Nozzle
  • Volume and Shape
  • Heat Transfer Distribution
  • Cooling of Thrust Chambers
  • Hydraulic Losses in the Cooling Passage
  • Thrust Chamber Wall Loads and Stresses
  • 8.3. Low-Thrust Rocket Thrust Chambers or Thrusters
  • 8.4. Materials and Fabrication
  • 8.5. Heat Transfer Analysis
  • General Steady-State Heat Transfer Relations
  • Transient Heat Transfer Analysis
  • Steady-State Transfer to Liquids in Cooling Jacket
  • Radiation
  • 8.6. Starting and Ignition
  • 8.7. Useful Life of Thrust Chambers
  • 8.8. Random Variable Thrust
  • 8.9. Sample Thrust Chamber Design Analysis
  • Symbols
  • Greek Letters
  • Subscripts
  • Problems
  • References
  • Chapter 9: Liquid Propellant Combustion and Its Stability
  • 9.1. Combustion Process
  • Injection/Atomization Zone
  • Rapid Combustion Zone
  • Streamtube Combustion Zone
  • 9.2. Analysis and Simulation
  • 9.3. Combustion Instability
  • Rating Techniques
  • Control of Instabilities
  • Problems
  • References
  • Chapter 10: Turbopumps and Their Gas Supplies
  • 10.1. Introduction
  • 10.2. Descriptions of Several Turbopumps
  • 10.3. Selection of Turbopump Configuration
  • 10.4. Flow, Shaft Speeds, Power, and Pressure Balances
  • 10.5. Pumps
  • Classification and Description
  • Pump Parameters
  • Influence of Propellants
  • 10.6. Turbines
  • Classification and Description
  • Turbine Performance and Design Considerations
  • 10.7. Approach to Turbopump Preliminary Design
  • 10.8. Gas Generators and Preburners
  • Symbols
  • Greek Letters
  • Subscripts
  • Problems
  • References
  • Chapter 11: Engine Systems, Controls, and Integration
  • 11.1. Propellant Budget.
  • 11.2. Performance of Complete or Multiple Rocket Propulsion Systems
  • 11.3. Engine Design
  • 11.4. Engine Controls
  • Control of Engine Starting and Thrust Buildup
  • Automatic Controls
  • Control by Computer
  • 11.5. Engine System Calibration
  • Engine Health Monitoring System
  • 11.6. System Integration and Engine Optimization
  • Symbols
  • Greek Letters
  • Subscripts
  • Problems
  • References
  • Chapter 12: Solid Propellant Rocket Motor Fundamentals
  • 12.1. Basic Relations and Propellant Burning Rate
  • Mass Flow Relations
  • Burning Rate Relation with Pressure
  • Burning Rate Relation with Ambient Temperature (Tb)
  • Variable Burning Rate Exponent n
  • Burning Enhancement by Erosion
  • Other Burning Rate Enhancements
  • 12.2. Other Performance Issues
  • 12.3. Propellant Grain and Grain Configuration
  • Slivers
  • 12.4. Propellant Grain Stress and Strain
  • Material Characterization
  • Structural Design
  • 12.5. Attitude Control and Side Maneuvers with Solid Propellant Rocket Motors
  • Symbols
  • Greek Letters
  • Subscripts
  • Problems
  • References
  • Chapter 13: Solid Propellants
  • 13.1. Classification
  • 13.2. Propellant Characteristics
  • Inadvertent Ignition
  • Aging and Useful Life
  • Case Overpressure and Failure
  • Insensitive Munitions
  • Upper Pressure Limit
  • Toxicity
  • Safety Rules
  • 13.3. Hazards
  • Inadvertent Ignition
  • Aging and Useful Life
  • Case Overpressure and Failure
  • Insensitive Munitions
  • Upper Pressure Limit
  • Toxicity
  • Safety Rules
  • 13.4. Propellant Ingredients
  • Inorganic Oxidizers
  • Fuels
  • Binders
  • Burning-Rate Modifiers
  • Plasticizers
  • Curing Agents or Crosslinkers
  • Energetic Binders and Plasticizers
  • Organic Oxidizers or Explosives
  • Additives
  • Particle-Size Parameters
  • 13.5. Other Propellant Categories
  • Gas Generator Propellants
  • Smokeless or Low-Smoke Propellant.
  • Igniter Propellants
  • 13.6. Liners, Insulators, and Inhibitors
  • 13.7. Propellant Processing and Manufacture
  • Problems
  • References
  • Chapter 14: Solid Propellant Combustion and Its Stability
  • 14.1. Physical and Chemical Processes
  • 14.2. Ignition Process
  • 14.3. Extinction or Thrust Termination
  • 14.4. Combustion Instability
  • Acoustic Instabilities
  • Analytical Models and Simulation of Combustion Stability
  • Combustion Stability Assessment, Remedy, and Design
  • Vortex-Shedding Instability
  • Problems
  • References
  • Chapter 15: Solid Rocket Motor Components and Design
  • 15.1. Rocket Motor Case
  • Metal Cases
  • Wound-Filament-Reinforced Plastic Cases
  • 15.2. Nozzles
  • Classification
  • Design and Construction
  • Heat Absorption and Nozzle Materials
  • 15.3. Igniter Hardware
  • Pyrotechnic Igniters
  • Pyrogen Igniters
  • Igniter Analysis and Design
  • 15.4. Rocket Motor Design Approach
  • Problems
  • References
  • Chapter 16: Hybrid Propellants Rocket Propulsion
  • 16.1. Applications and Propellants
  • 16.2. Interior Hybrid Motor Ballistics
  • 16.3. Performance Analysis and Grain Configuration
  • Dynamic Behavior
  • 16.4. Design Example
  • 16.5. Combustion Instability
  • Symbols
  • Greek Letters
  • Subscripts
  • Problems
  • References
  • Chapter 17: Electric Propulsion
  • 17.1. Ideal Flight Performance
  • 17.2. Electrothermal Thrusters
  • Resistojets
  • Arcjets
  • 17.3. Nonthermal Electrical Thrusters
  • Electrostatic Devices
  • Basic Relationships for Electrostatic Thrusters
  • Electromagnetic Thrusters
  • 17.4. Optimum Flight Performance
  • 17.5. Mission Applications
  • 17.6. Electric Space-Power Supplies and Power-Conditioning Systems
  • Power Generation Units
  • Power-Conditioning Equipment (PCU or PPU)
  • Symbols
  • Greek Letters
  • Problems
  • References
  • Chapter 18: Thrust Vector Control.
  • 18.1. TVC Mechanisms with a Single Nozzle.

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