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Cover
Title Page
Copyright
Preface
Chapter 1: Classification
1. 1.1. Duct Jet Propulsion
2. 1.2. Rocket Propulsion
3. 1.3. Applications of Rocket Propulsion
4. References
Chapter 2: Definitions and Fundamentals
1. 2.1. Definitions
2. 2.2. Thrust
3. 2.3. Exhaust Velocity
4. 2.4. Energy and Efficiencies
5. 2.5. Multiple Propulsion Systems
6. 2.6. Typical Performance Values
7. 2.7. Variable Thrust
8. Symbols
9. Problems
10. References
Chapter 3: Nozzle Theory and Thermodynamic Relations
1. 3.1. Ideal Rocket Propulsion Systems
2. 3.2. Summary of Thermodynamic Relations
3. 3.3. Isentropic Flow through Nozzles
4. 3.4. Nozzle Configurations
5. 3.5. Real Nozzles
6. 3.6. Nozzle Alignment
7. Symbols
8. Problems
9. References
Chapter 4: Flight Performance
1. 4.1. Gravity-Free Drag-Free Space Flight
2. 4.2. Forces Acting on a Vehicle in the Atmosphere
3. 4.3. Basic Relations of Motion
4. 4.4. Space Flight
5. 4.5. Space Flight Maneuvers
6. 4.6. Effect of Propulsion System on Vehicle Performance
7. 4.7. Flight Vehicles
8. 4.8. Military Missiles
9. 4.9. Flight Stability
10. Symbols
11. Problems
12. References
Chapter 5: Chemical Rocket Propellant Performance Analysis
1. 5.1. Background and Fundamentals
2. 5.2. Analysis of Chamber or Motor Case Conditions
3. 5.3. Analysis of Nozzle Expansion Processes
4. 5.4. Computer-Assisted Analysis
5. 5.5. Results of Thermochemical Calculations
6. Symbols
7. Problems
8. References
Chapter 6: Liquid Propellant Rocket Engine Fundamentals
1. 6.1. Types of Propellants
2. 6.2. Propellant Tanks
3. 6.3. Propellant Feed Systems
4. 6.4. Gas Pressure Feed Systems
5. 6.5. Tank Pressurization
6. 6.6. Turbopump Feed Systems and Engine Cycles
7. 6.7. Rocket Engines for Maneuvering, Orbit Adjustments, or Attitude Control
8. 6.8. Engine Families
9. 6.9. Valves and Pipelines
10. 6.10. Engine Support Structure
11. Symbols
12. Problems
13. References
Chapter 7: Liquid Propellants
1. 7.1. Propellant Properties
2. 7.2. Liquid Oxidizers
3. 7.3. Liquid Fuels
4. 7.4. Liquid Monopropellants
5. 7.5. Gaseous Propellants
6. 7.6. Safety and Environmental Concerns
7. Symbols
8. Problems
9. References
Chapter 8: Thrust Chambers
1. 8.1. Injectors
2. 8.2. Combustion Chamber and Nozzle
3. 8.3. Low-Thrust Rocket Thrust Chambers or Thrusters
4. 8.4. Materials and Fabrication
5. 8.5. Heat Transfer Analysis
6. 8.6. Starting and Ignition
7. 8.7. Useful Life of Thrust Chambers
8. 8.8. Random Variable Thrust
9. 8.9. Sample Thrust Chamber Design Analysis
10. Symbols
11. Problems
12. References
Chapter 9: Liquid Propellant Combustion and Its Stability
1. 9.1. Combustion Process
2. 9.2. Analysis and Simulation
3. 9.3. Combustion Instability
4. Problems
5. References
Chapter 10: Turbopumps and Their Gas Supplies
1. 10.1. Introduction
2. 10.2. Descriptions of Several Turbopumps
3. 10.3. Selection of Turbopump Configuration
4. 10.4. Flow, Shaft Speeds, Power, and Pressure Balances
5. 10.5. Pumps
6. 10.6. Turbines
7. 10.7. Approach to Turbopump Preliminary Design
8. 10.8. Gas Generators and Preburners
9. Symbols
10. Problems
11. References
Chapter 11: Engine Systems, Controls, and Integration
1. 11.1. Propellant Budget
2. 11.2. Performance of Complete or Multiple Rocket Propulsion Systems
3. 11.3. Engine Design
4. 11.4. Engine Controls
5. 11.5. Engine System Calibration
6. 11.6. System Integration and Engine Optimization
7. Symbols
8. Problems
9. References
Chapter 12: Solid Propellant Rocket Motor Fundamentals
1. 12.1. Basic Relations and Propellant Burning Rate
2. 12.2. Other Performance Issues
3. 12.3. Propellant Grain and Grain Configuration
4. 12.4. Propellant Grain Stress and Strain
5. 12.5. Attitude Control and Side Maneuvers with Solid Propellant Rocket Motors
6. Symbols
7. Problems
8. References
Chapter 13: Solid Propellants
1. 13.1. Classification
2. 13.2. Propellant Characteristics
3. 13.3. Hazards
4. 13.4. Propellant Ingredients
5. 13.5. Other Propellant Categories
6. 13.6. Liners, Insulators, and Inhibitors
7. 13.7. Propellant Processing and Manufacture
8. Problems
9. References
Chapter 14: Solid Propellant Combustion and Its Stability
1. 14.1. Physical and Chemical Processes
2. 14.2. Ignition Process
3. 14.3. Extinction or Thrust Termination
4. 14.4. Combustion Instability
5. Problems
6. References
Chapter 15: Solid Rocket Motor Components and Design
1. 15.1. Rocket Motor Case
2. 15.2. Nozzles
3. 15.3. Igniter Hardware
4. 15.4. Rocket Motor Design Approach
5. Problems
6. References
Chapter 16: Hybrid Propellants Rocket Propulsion
1. 16.1. Applications and Propellants
2. 16.2. Interior Hybrid Motor Ballistics
3. 16.3. Performance Analysis and Grain Configuration
4. 16.4. Design Example
5. 16.5. Combustion Instability
6. Symbols
7. Problems
8. References
Chapter 17: Electric Propulsion
1. 17.1. Ideal Flight Performance
2. 17.2. Electrothermal Thrusters
3. 17.3. Nonthermal Electrical Thrusters
4. 17.4. Optimum Flight Performance
5. 17.5. Mission Applications
6. 17.6. Electric Space-Power Supplies and Power-Conditioning Systems
7. Symbols
8. Problems
9. References
Chapter 18: Thrust Vector Control
1. 18.1. TVC Mechanisms with a Single Nozzle
2. 18.2. TVC with Multiple Thrust Chambers or Nozzles
3. 18.3. Testing
4. 18.4. Integration with Vehicle
5. Problems
6. References
Chapter 19: Selection of Rocket Propulsion Systems
1. 19.1. Selection Process
2. 19.2. Criteria for Selection
3. 19.3. Interfaces
4. 19.4. Cost Reduction
5. References
Chapter 20: Rocket Exhaust Plumes
1. 20.1. Plume Appearance and Flow Behavior
2. 20.2. Plume Effects
3. 20.3. Analysis and Mathematical Simulation
4. Problems
5. References
Chapter 21: Rocket Testing
1. 21.1. Types of Tests
2. 21.2. Test Facilities and Safeguards
3. 21.3. Instrumentation and Data Management
4. 21.4. Flight Testing
5. 21.5. Postaccident Procedures
6. References
Appendix 1: Conversion Factors and Constants
1. Conversion Factors (arranged alphabetically)
2. Constants
Appendix 2: Properties of the Earth's Standard Atmosphere
Appendix 3: Summary of Key equations for Ideal Chemical Rockets
Index
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