Rocket Propulsion Elements
- Nyhet
Inbunden, Engelska, 2026
Av George P. Sutton, Oscar Biblarz, James H. Morehart, George P. (Massachusetts Institute of Technology) Sutton, Oscar (Naval Postgraduate School) Biblarz
1 989 kr
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Produktinformation
- Utgivningsdatum2026-05-18
- FormatInbunden
- SpråkEngelska
- Antal sidor720
- Upplaga10
- FörlagJohn Wiley & Sons Inc
- ISBN9781394187201
Tillhör följande kategorier
- PREFACE TO THE 10TH EDITION xvIn Memoriam George Paul Sutton (1920–2020) / xvii1 Classification 11.1. Jet Propulsion / 21.2. Rocket Propulsion / 5Chemical Rocket Propulsion / 5Combinations of Air-Breathing Jet Engines and Rocket Motors / 8Nuclear Rocket Engines / 10Electric Rocket Propulsion (EP) / 11Other Rocket Propulsion Concepts / 12International Rocket Propulsion Effort / 131.3. Applications of Rocket Propulsion / 14Space Launch Vehicles / 14Spacecraft / 19Military and Other Applications / 20References / 232 Definitions and Fundamentals 252.1. Definitions / 252.2. Thrust / 292.3. Exhaust Velocity / 312.4. Energy and Efficiencies / 322.5. Multiple Parallel Propulsion Systems / 352.6. Typical Performance Values / 362.7. Variable Thrust / 37Symbols / 38Greek Letters / 39Problems / 39References / 413 Nozzle Theory and Thermodynamic Relations 423.1. Ideal Rocket Propulsion Systems / 423.2. Summary of Thermodynamic Relations / 443.3. Isentropic Flow Through Nozzles / 47Velocity / 48Nozzle Flow and Throat Condition / 52Thrust and Thrust Coefficient / 56Characteristic Velocity and Specific Impulse / 59Under- and Over-expanded Nozzles / 61Influence of Chamber Geometry / 653.4. Nozzle Configurations / 66Cone- and Bell-Shaped Nozzles / 663.5. Real Nozzles / 73Boundary Layers / 73Multiphase Flow / 75Other Phenomena and Losses / 76Performance Correction Factors / 763.6. Nozzle Alignment / 81Symbols / 82Greek Letters / 83Subscripts / 83Problems / 84References / 864 Flight Performance 884.1. Gravity-Free Drag-Free Space Flight / 884.2. Forces Acting on a Vehicle in the Atmosphere / 914.3. Basic Relations of Motion / 944.4. Space Flight / 100Elliptical Orbits / 103Deep Space / 106Perturbations / 107Mission Velocity / 1104.5. Space Flight Maneuvers / 112Reaction Control System (RCS) / 1154.6. Effect of Propulsion System on Vehicle Performance / 1174.7. Flight Vehicles / 119Multistage Vehicles in Series / 120Stage Separation / 121Launch Vehicles / 1244.8. Military Missiles / 1274.9. Flight Stability / 130Symbols / 131Greek Letters / 132Subscripts / 133Problems / 133References / 1345 Chemical Rocket Propellant Performance Analysis 1365.1. Background and Fundamentals / 1375.2. Analysis of Chamber or Motor Case Conditions / 1435.3. Analysis of Nozzle Expansion Processes / 1475.4. Computer-Assisted Analysis / 1505.5. Results of Thermochemical Calculations / 151Symbols / 162Greek Letters / 163Subscripts / 163Problems / 163References / 1646 Liquid Propellant Rocket Engine Fundamentals 1656.1. Types of Propellants / 1686.2. Propellant Tanks / 1716.3. Propellant Feed Systems / 176Local Pressures and Flows / 1776.4. Gas Pressure Feed Systems / 1786.5. Tank Pressurization / 183Factors Influencing the Required Mass of Pressurizing Gas / 185Simplified Analysis for the Mass of Pressurizing Gas / 1866.6. Turbopump Feed Systems and Engine Cycles / 187Engine Cycles / 1886.7. Rocket Engines for Maneuvering, Orbit Adjustments, or Attitude Control / 1966.8. Engine Families / 1996.9. Valves and Pipelines / 2006.10. Engine Support Structure / 204Symbols / 205Subscripts / 206Problems / 206References / 2087 Liquid Propellants 2107.1. Propellant Properties / 214Economic Factors / 214Performance of Propellants / 214Common Physical Hazards / 215Desirable Physical Properties of Propellants / 217Ignition, Combustion, and Flame Properties / 218Property Variations and Specifications / 219Additives / 2197.2. Liquid Oxidizers / 219Liquid Oxygen (O2) (LOX) / 220Hydrogen Peroxide (H2O2) / 221Nitric Acid (HNO3) / 221Nitrogen Tetroxide (N2O4 or NTO) / 222Nitrous Oxide (N2O) / 222Oxidizer Cleaning Process / 2237.3. Liquid Fuels / 223Hydrocarbon Fuels / 223Liquid Hydrogen / 224Hydrazine (N2H4) / 225Unsymmetrical Dimethylhydrazine [(CH3)2NNH2] / 226Monomethylhydrazine (CH3NHNH2) / 226Metallic Hydrogen / 2267.4. Liquid Monopropellants / 227Hydrazine as a Monopropellant / 2277.5. Gaseous Propellants / 2307.6. Safety and Environmental Concerns / 231Symbols / 232Greek Letters / 232Problems / 232References / 2348 Thrust Chambers 2378.1. Injectors / 237Injector Flow Characteristics / 246Factors Influencing Injector Behavior / 2488.2. Combustion Chamber and Nozzle / 250Volume and Shape / 250Heat Transfer Distribution / 252Cooling of Thrust Chambers / 253Hydraulic Losses in the Cooling Passage / 258Thrust Chamber Wall Loads and Stresses / 2598.3. Low-Thrust Rocket Thrust Chambers or Thrusters / 2628.4. Materials and Fabrication / 265Additive Manufacturing of Rocket Engine Components / 2718.5. Heat Transfer Analysis / 272General Steady-State Heat Transfer Relations / 272Transient Heat Transfer Analysis / 276Steady-State Transfer to Liquids in Cooling Channels / 278Radiation / 2818.6. Start-up and Ignition / 2828.7. Useful Life of Thrust Chambers / 2858.8. Random Variable Thrust / 2868.9. Sample Thrust Chamber Design Analysis / 287Symbols / 296Greek Letters / 297Subscripts / 297Problems / 297References / 3009 Liquid Propellant Combustion and its Stability 3039.1. Combustion Process / 303Injection/Atomization zone / 304Rapid Combustion Zone / 306Streamtube Combustion Zone / 3069.2. Analysis and Simulation / 3069.3. Combustion Instability / 307Rating Techniques / 313Control of Instabilities / 314Symbols / 317Problems / 317References / 31810 Turbopumps and their Gas Supplies 32010.1. Introduction / 32010.2. Descriptions of Several Turbopump Assemblies / 32110.3. Selection of Turbopump Configuration / 32510.4. Flow, Shaft Speeds, Power, and Pressure Balances / 32910.5. Pumps / 330Classification and Description / 330Pump Parameters / 331Influence of Propellants / 33610.6. Turbines / 338Classification and Description / 338Turbine Performance and Design Considerations / 34010.7. Approach to Turbopump Preliminary Design / 34110.8. Gas Generators and Preburners / 344Symbols / 345Greek Letters / 346Subscripts / 346Problems / 346References / 34711 Engine Systems, Controls, and Integration 35011.1. Propellant Budget / 35011.2. Performance of Complete or Multiple Rocket Propulsion Systems / 35211.3. Engine Design / 35511.4. Engine Controls / 361Control of Engine Starting and Thrust Buildup / 363Automatic Controls / 368Control by Computer / 36911.5. Engine System Calibration / 371Engine Health Monitoring System / 37511.6. System Integration and Engine Optimization / 377Symbols / 378Greek Letters / 378Subscripts / 378Problems / 378References / 37912 Solid-propellant Rocket Motor Fundamentals 38112.1. Basic Relations and Propellant Burning Rate / 388Mass Flow Relations / 390Burning Rate Relation with Pressure / 391Burning Rate Relation with Ambient Temperature (Tb) / 394Variable Burning Rate Exponent n / 397Burning Enhancement by Erosion / 398Other Burning Rate Enhancements / 40012.2. Other Performance Issues / 40112.3. Propellant Grain and Grain Configuration / 405Slivers / 41212.4. Propellant Grain Stress and Strain / 413Material Characterization / 414Structural Design / 41612.5. Attitude Control and Side Maneuvers with Solid-Propellant Rocket Motors / 422Symbols / 423Greek Letters / 425Subscripts / 425Problems / 425References / 42713 Solid Rocket Propellants 43113.1. Classification / 43113.2. Propellant Characteristics / 43613.3. Hazards / 442Inadvertent Ignition / 442Aging and Useful Life / 443Case Overpressure and Failure / 443Detonation Versus Deflagration / 444Hazard Classification / 444Insensitive Munitions / 445Upper Pressure Limit / 447Toxicity / 447Safety Rules / 44713.4. Propellant Ingredients / 447Inorganic Oxidizers / 452Fuels / 453Binders / 453Burning-Rate Modifiers / 454Plasticizers / 454Curing Agents or Crosslinkers / 454Energetic Binders and Plasticizers / 455Organic Oxidizers or Explosives / 455Additives / 456Particle-Size Parameters / 45613.5. Other Propellant Categories / 458Gas Generator Propellants / 458Smokeless or Low-Smoke Propellant / 459Igniter Propellants / 46013.6. Liners, Insulators, and Inhibitors / 46013.7. Propellant Processing and Manufacture / 463Symbols / 466Greek Letters / 466Problems / 466References / 46814 Solid Propellant Combustion and its Stability 47214.1. Physical and Chemical Processes / 47214.2. Ignition Process / 47514.3. Extinction or Thrust Termination / 47614.4. Combustion Instability / 478Acoustic Instabilities / 478Analytical Models and Simulation of Combustion Stability / 481Combustion Stability Assessment, Remedy, and Design / 482Vortex-Shedding Instability / 484Problems / 485References / 48515 Solid Rocket Motor Components and Design 48815.1. Rocket Motor Case / 488Metal Cases / 491Wound-Filament-Reinforced Plastic Cases / 49415.2. Nozzles / 496Classification / 496Design and Construction / 498Heat Absorption and Nozzle Materials / 50215.3. Igniter Hardware / 507Pyrotechnic Igniters / 508Pyrogen Igniters / 509Igniter Analysis and Design / 51115.4. Rocket Motor Design Approach / 512Symbols / 518Greek Letters / 518Subscripts / 518Problems / 519References / 52016 Hybrid Propellants Rocket Propulsion 52316.1. Applications and Propellants / 52516.2. Hybrid Rocket Engine Interior Ballistics / 52816.3. Performance Analysis and Grain Configuration / 531Dynamic Behavior / 53316.4. Design Example / 53516.5. Combustion Instability / 539Symbols / 542Greek Letters / 543Problems / 543References / 54417 Electric Propulsion 54717.1. Ideal Flight Performance / 55217.2. Electrothermal Thrusters / 556Resistojets / 556Arcjets / 55817.3. Nonthermal Electrical Thrusters / 562Electrostatic Devices / 562Basic Relationships for Electrostatic Thrusters / 563Electromagnetic Thrusters / 56917.4. Optimum Flight Performance / 57517.5. Mission Applications / 57917.6. Electric Space-power Supplies and Power-conditioning Systems / 580Power Generation Units / 581Power-Conditioning Equipment (PCU or PPU) / 583Symbols / 584Greek Letters / 585Problems / 586References / 588References for Table: 17–7 / 59018 Thrust Vector Control (TVC) 59118.1. TVC Mechanisms with a Single Nozzle / 59318.2. TVC with Multiple Thrust Chambers or Nozzles / 60118.3. Testing / 60318.4. Integration with Vehicle / 605Problems / 606References / 60619 Selection of Rocket Propulsion Systems 60819.1. Selection Process / 61019.2. Criteria for Selection / 61419.3. Interfaces / 61619.4. Cost Reduction / 61619.5. Optimization Results / 618References / 62020 Rocket Exhaust Plumes 62120.1. Plume Appearance and Flow Behavior / 621Spectral Distribution of Radiation / 627Multiple Nozzles / 630Plume Signature / 630Vehicle Base Geometry and Recirculation / 631Compression and Expansion Waves / 63220.2. Plume Effects / 633Smoke and Vapor Trails / 633Toxicity / 634Noise / 634Spacecraft Surface Contamination / 635Radio Signal Attenuation / 636Plume Impingement on Structures / 637Heat Transfer to Clusters of Liquid Propellant Rocket Engines / 63720.3. Analysis and Mathematical Simulation / 638Problems / 638References / 63921 Rocket Testing 64121.1. Types of Tests / 64121.2. Test Facilities and Safeguards / 643Monitoring the Environment and Controlling Toxic Materials / 64621.3. Instrumentation and Data Management / 648Measurement System Terminology / 649Test Measurements / 650Health Monitoring System (HMS) / 65121.4. Flight Testing / 65221.5. Postaccident Procedures / 652Symbols / 653References / 653Appendix 1 Conversion Factors and Constants 655Conversion Factors (Arranged Alphabetically) / 655Constants / 657Appendix 2 Properties of the Earth’s Standard Atmosphere 658Appendix 3 Summary of Key Equations for Ideal Chemical Rockets 659Appendix 4 Rockets Book Calculator 662Index 665
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