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• Cover
• Title Page
• Copyright
• Preface
• Chapter 1: Classification
• 1.1. Duct Jet Propulsion
• 1.2. Rocket Propulsion
• 1.3. Applications of Rocket Propulsion
• 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
• 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
• 3.4. Nozzle Configurations
• 3.5. Real Nozzles
• 3.6. Nozzle Alignment
• Symbols
• 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
• 4.5. Space Flight Maneuvers
• 4.6. Effect of Propulsion System on Vehicle Performance
• 4.7. Flight Vehicles
• 4.8. Military Missiles
• 4.9. Flight Stability
• Symbols
• 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
• Problems
• References
• Chapter 6: Liquid Propellant Rocket Engine Fundamentals
• 6.1. Types of Propellants
• 6.2. Propellant Tanks
• 6.3. Propellant Feed Systems
• 6.4. Gas Pressure Feed Systems
• 6.5. Tank Pressurization
• 6.6. Turbopump Feed Systems and 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
• Problems
• References
• Chapter 7: Liquid Propellants
• 7.1. Propellant Properties
• 7.2. Liquid Oxidizers
• 7.3. Liquid Fuels
• 7.4. Liquid Monopropellants
• 7.5. Gaseous Propellants
• 7.6. Safety and Environmental Concerns
• Symbols
• Problems
• References
• Chapter 8: Thrust Chambers
• 8.1. Injectors
• 8.2. Combustion Chamber and Nozzle
• 8.3. Low-Thrust Rocket Thrust Chambers or Thrusters
• 8.4. Materials and Fabrication
• 8.5. Heat Transfer Analysis
• 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
• Problems
• References
• Chapter 9: Liquid Propellant Combustion and Its Stability
• 9.1. Combustion Process
• 9.2. Analysis and Simulation
• 9.3. Combustion Instability
• 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
• 10.6. Turbines
• 10.7. Approach to Turbopump Preliminary Design
• 10.8. Gas Generators and Preburners
• Symbols
• 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
• 11.5. Engine System Calibration
• 11.6. System Integration and Engine Optimization
• Symbols
• Problems
• References
• Chapter 12: Solid Propellant Rocket Motor Fundamentals
• 12.1. Basic Relations and Propellant Burning Rate
• 12.2. Other Performance Issues
• 12.3. Propellant Grain and Grain Configuration
• 12.4. Propellant Grain Stress and Strain
• 12.5. Attitude Control and Side Maneuvers with Solid Propellant Rocket Motors
• Symbols
• Problems
• References
• Chapter 13: Solid Propellants
• 13.1. Classification
• 13.2. Propellant Characteristics
• 13.3. Hazards
• 13.4. Propellant Ingredients
• 13.5. Other Propellant Categories
• 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
• Problems
• References
• Chapter 15: Solid Rocket Motor Components and Design
• 15.1. Rocket Motor Case
• 15.2. Nozzles
• 15.3. Igniter Hardware
• 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
• 16.4. Design Example
• 16.5. Combustion Instability
• Symbols
• Problems
• References
• Chapter 17: Electric Propulsion
• 17.1. Ideal Flight Performance
• 17.2. Electrothermal Thrusters
• 17.3. Nonthermal Electrical Thrusters
• 17.4. Optimum Flight Performance
• 17.5. Mission Applications
• 17.6. Electric Space-Power Supplies and Power-Conditioning Systems
• Symbols
• Problems
• References
• Chapter 18: Thrust Vector Control
• 18.1. TVC Mechanisms with a Single Nozzle
• 18.2. TVC with Multiple Thrust Chambers or Nozzles
• 18.3. Testing
• 18.4. Integration with Vehicle
• Problems
• References
• Chapter 19: Selection of Rocket Propulsion Systems
• 19.1. Selection Process
• 19.2. Criteria for Selection
• 19.3. Interfaces
• 19.4. Cost Reduction
• References
• Chapter 20: Rocket Exhaust Plumes
• 20.1. Plume Appearance and Flow Behavior
• 20.2. Plume Effects
• 20.3. Analysis and Mathematical Simulation
• Problems
• References
• Chapter 21: Rocket Testing
• 21.1. Types of Tests
• 21.2. Test Facilities and Safeguards
• 21.3. Instrumentation and Data Management
• 21.4. Flight Testing
• 21.5. Postaccident Procedures
• References
• Appendix 1: Conversion Factors and Constants
• Conversion Factors (arranged alphabetically)
• Constants
• Appendix 2: Properties of the Earth’s Standard Atmosphere
• Appendix 3: Summary of Key equations for Ideal Chemical Rockets
• Index
• Wiley End User License Agreement