Rocket Propulsion Elements
Höfundar: George P. Sutton, Oscar Biblarz
9.690 kr.
Lýsing:
The classic rocket propulsion text, updated with the industry's latest advances Rocket Propulsion Elements is the definitive guide for students and professionals, with comprehensive coverage from one of the field's most respected authorities. Combining fundamental concepts with industry applications, this book provides a practical introduction to rocket propulsion principles, mechanisms, and design as applied to guided missiles, space flight, satellite flight, and more.
This new ninth edition has been updated to cover the latest advances in the field, including new technologies in systems design, materials, propellants, applications, and manufacturing, with an emphasis on system types commonly used around the world today. Broad in scope yet rich in detail, the discussion covers a wide range of topics from engine performance to propellant chemistry to provide a clear, comprehensive resource for all aspects of rocket propulsion.
Rocket propulsion technology is advancing quickly, driven by a global upsurge in defense spending. Those who design these systems require a strong grounding in the physics and chemistry of rocket propulsion systems, as well as an up-to-date understanding of current industry applications. This book delivers the fundamentals with the guidance of an industry-leading expert. Delve into rockets' mechanical systems and design Develop a working knowledge of propellant chemistry Understand aerodynamics, flight performance, and industry applications Learn the latest advances in materials, systems, propellants, and more This book's unique strength is the presentation of fundamental concepts through the lens of modern applications.
Annað
- Höfundar: George P. Sutton, Oscar Biblarz
- Útgáfa:9
- Útgáfudagur: 2016-11-30
- Hægt að prenta út 10 bls.
- Hægt að afrita 2 bls.
- Format:ePub
- ISBN 13: 9781118753910
- Print ISBN: 9781118753651
- ISBN 10: 1118753917
Efnisyfirlit
- 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
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- Gerð : 208
- Höfundur : 12370
- Útgáfuár : 2016
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