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Rocket Propulsion Elements George P. Sutton (Massachusetts Institute of Technology Rocketdyne, a Division of Rockwell International Corporation)

Rocket Propulsion Elements By George P. Sutton (Massachusetts Institute of Technology Rocketdyne, a Division of Rockwell International Corporation)

Summary

THE DEFINITIVE INTRODUCTION TO ROCKET PROPULSION THEORY AND APPLICATIONS The recent upsurge in global government and private spending and in space flight events has resulted in many novel applications of rocket propulsion technology.

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Rocket Propulsion Elements Summary

Rocket Propulsion Elements by George P. Sutton (Massachusetts Institute of Technology Rocketdyne, a Division of Rockwell International Corporation)

ROCKET PROPULSION ELEMENTS

THE DEFINITIVE INTRODUCTION TO ROCKET PROPULSION THEORY AND APPLICATIONS

The recent upsurge in global government and private spending and in space flight events has resulted in many novel applications of rocket propulsion technology. Rocket Propulsion Elements remains the definitive guide to the field, providing a comprehensive introduction to essential concepts and applications. Led by industry veteran George P. Sutton and by Professor Oscar Biblarz, this book provides interdisciplinary coverage including thermodynamics, aerodynamics, flight performance, propellant chemistry and more.

This thoroughly revised ninth edition includes discussion and analysis of recent advances in the field, representing an authoritative reference for students and working engineers alike. In any engineering field, theory is only as useful as it is practical; this book emphasizes relevant real-world applications of fundamental concepts to link thinking and doing. This book will help readers:

  • Understand the physics of flight and the chemistry of propulsion
  • Analyze liquid, solid, gas, and hybrid propellants, and the engines they fuel
  • Consider high-temperature combustion, stability, and the principles of electric and chemical propulsion
  • Dissect the workings of systems in common use around the world today
  • Delve into the latest advances in materials, systems, propellants, and more

Broad in scope, rich in detail, and clear in explanation, this seminal work provides an unparalleled foundation in aerospace engineering topics. Learning through the lens of modern applications untangles complex topics and helps students fully grasp the intricacies on a more intuitive level. Rocket Propulsion Elements, Ninth Edition merges information and utility building a solid foundation for innovation.

About George P. Sutton (Massachusetts Institute of Technology Rocketdyne, a Division of Rockwell International Corporation)

GEORGE P. SUTTON is an acknowledged expert on rocket propulsion, and the former Executive Director of Engineering at Rocketdyne (now Aerojet Rocketdyne), and Laboratory Associate at Lawrence Livermore National Laboratory.

OSCAR BIBLARZ is a Professor Emeritus in the Department of Mechanical and Aerospace Engineering at the Naval Postgraduate School in Monterey, California.

Table of Contents

Preface xvii

1 Classification 1

1.1. Duct Jet Propulsion 2

1.2. Rocket Propulsion 4

Chemical Rocket Propulsion 5

Combinations of Ducted Jet Engines and Rocket Engines 9

Nuclear Rocket Engines 10

Electric Rocket Propulsion 10

Other Rocket Propulsion Concepts 12

International Rocket Propulsion Effort 13

1.3. Applications of Rocket Propulsion 14

Space Launch Vehicles 14

Spacecraft 20

Military and Other Applications 21

References 24

2 Definitions and Fundamentals 26

2.1. Definitions 26

2.2. Thrust 31

2.3. Exhaust Velocity 33

2.4. Energy and Efficiencies 35

2.5. Multiple Propulsion Systems 38

2.6. Typical Performance Values 39

2.7. Variable Thrust 40

Symbols 41

Problems 42

References 44

3 Nozzle Theory and Thermodynamic Relations 45

3.1. Ideal Rocket Propulsion Systems 45

3.2. Summary of Thermodynamic Relations 47

3.3. Isentropic Flow through Nozzles 51

Velocity 52

Nozzle Flow and Throat Condition 57

Thrust and Thrust Coefficient 61

Characteristic Velocity and Specific Impulse 63

Under- and Overexpanded Nozzles 67

Influence of Chamber Geometry 72

3.4. Nozzle Configurations 73

Cone- and Bell-Shaped Nozzles 75

3.5. Real Nozzles 81

Boundary Layers 82

Multiphase Flow 83

Other Phenomena and Losses 85

Performance Correction Factors 85

Four Performance Parameters 89

3.6. Nozzle Alignment 91

Symbols 93

Problems 94

References 97

4 Flight Performance 99

4.1. Gravity-Free Drag-Free Space Flight 99

4.2. Forces Acting on a Vehicle in the Atmosphere 104

4.3. Basic Relations of Motion 106

4.4. Space Flight 113

Elliptical Orbits 116

Deep Space 120

Perturbations 121

Mission Velocity 125

4.5. Space Flight Maneuvers 127

Reaction Control System 131

4.6. Effect of Propulsion System on Vehicle Performance 133

4.7. Flight Vehicles 136

Multistage Vehicles 136

Stage Separation 138

Launch Vehicles 141

4.8. Military Missiles 144

4.9. Flight Stability 147

Symbols 149

Problems 150

References 152

5 Chemical Rocket Propellant Performance Analysis 154

5.1. Background and Fundamentals 156

5.2. Analysis of Chamber or Motor Case Conditions 161

5.3. Analysis of Nozzle Expansion Processes 166

5.4. Computer-Assisted Analysis 171

5.5. Results of Thermochemical Calculations 172

Symbols 185

Problems 186

References 187

6 Liquid Propellant Rocket Engine Fundamentals 189

6.1. Types of Propellants 192

6.2. Propellant Tanks 196

6.3. Propellant Feed Systems 203

Local Pressures and Flows 203

6.4. Gas Pressure Feed Systems 205

6.5. Tank Pressurization 212

Factors Influencing the Required Mass of Pressurizing Gas 214

Simplified Analysis for the Mass of Pressurizing Gas 215

6.6. Turbopump Feed Systems and Engine Cycles 217

Engine Cycles 218

6.7. Rocket Engines for Maneuvering, Orbit Adjustments, or Attitude Control 229

6.8. Engine Families 232

6.9. Valves and Pipelines 233

6.10. Engine Support Structure 239

Symbols 239

Problems 240

References 242

7 Liquid Propellants 244

7.1. Propellant Properties 245

Economic Factors 245

Performance of Propellants 246

Common Physical Hazards 250

Desirable Physical Properties 252

Ignition, Combustion, and Flame Properties 254

Property Variations and Specifications 254

Additives 255

7.2. Liquid Oxidizers 255

Liquid Oxygen (O2) (LOX) 255

Hydrogen Peroxide (H2O2) 256

Nitric Acid (HNO3) 257

Nitrogen Tetroxide (N2O4) (NTO) 258

Nitrous Oxide (N2O) 259

Oxidizer Cleaning Process 259

7.3. Liquid Fuels 259

Hydrocarbon Fuels 260

Liquid Hydrogen 261

Hydrazine (N2H4) 262

Unsymmetrical Dimethylhydrazine [(CH3)2NNH2] 263

Monomethylhydrazine (CH3NHNH2) 263

7.4. Liquid Monopropellants 264

Hydrazine as a Monopropellant 264

7.5. Gaseous Propellants 266

7.6. Safety and Environmental Concerns 267

Symbols 268

Problems 268

References 269

8 Thrust Chambers 271

8.1. Injectors 276

Injector Flow Characteristics 280

Factors Influencing Injector Behavior 283

8.2. Combustion Chamber and Nozzle 285

Volume and Shape 285

Heat Transfer Distribution 288

Cooling of Thrust Chambers 289

Hydraulic Losses in the Cooling Passage 295

Thrust Chamber Wall Loads and Stresses 296

8.3. Low-Thrust Rocket Thrust Chambers or Thrusters 300

8.4. Materials and Fabrication 304

8.5. Heat Transfer Analysis 310

General Steady-State Heat Transfer Relations 311

Transient Heat Transfer Analysis 315

Steady-State Transfer to Liquids in Cooling Jacket 317

Radiation 321

8.6. Starting and Ignition 322

8.7. Useful Life of Thrust Chambers 325

8.8. Random Variable Thrust 326

8.9. Sample Thrust Chamber Design Analysis 328

Symbols 338

Problems 339

References 342

9 Liquid Propellant Combustion and Its Stability 344

9.1. Combustion Process 344

Injection/Atomization Zone 346

Rapid Combustion Zone 347

Streamtube Combustion Zone 348

9.2. Analysis and Simulation 348

9.3. Combustion Instability 349

Rating Techniques 357

Control of Instabilities 358

Problems 362

References 362

10 Turbopumps and Their Gas Supplies 365

10.1. Introduction 365

10.2. Descriptions of Several Turbopumps 366

10.3. Selection of Turbopump Configuration 371

10.4. Flow, Shaft Speeds, Power, and Pressure Balances 376

10.5. Pumps 378

Classification and Description 378

Pump Parameters 379

Influence of Propellants 385

10.6. Turbines 387

Classification and Description 387

Turbine Performance and Design Considerations 389

10.7. Approach to Turbopump Preliminary Design 390

10.8. Gas Generators and Preburners 393

Symbols 395

Problems 396

References 397

11 Engine Systems, Controls, and Integration 399

11.1. Propellant Budget 399

11.2. Performance of Complete or Multiple Rocket Propulsion Systems 401

11.3. Engine Design 403

11.4. Engine Controls 412

Control of Engine Starting and Thrust Buildup 413

Automatic Controls 419

Control by Computer 421

11.5. Engine System Calibration 423

Engine Health Monitoring System 428

11.6. System Integration and Engine Optimization 430

Symbols 431

Problems 432

References 433

12 Solid Propellant Rocket Motor Fundamentals 434

12.1. Basic Relations and Propellant Burning Rate 439

Mass Flow Relations 444

Burning Rate Relation with Pressure 445

Burning Rate Relation with Ambient Temperature (Tb) 449

Variable Burning Rate Exponent n 452

Burning Enhancement by Erosion 453

Other Burning Rate Enhancements 455

12.2. Other Performance Issues 457

12.3. Propellant Grain and Grain Configuration 462

Slivers 471

12.4. Propellant Grain Stress and Strain 472

Material Characterization 473

Structural Design 476

12.5. Attitude Control and Side Maneuvers with Solid Propellant Rocket Motors 483

Symbols 485

Problems 486

References 488

13 Solid Propellants 491

13.1. Classification 491

13.2. Propellant Characteristics 497

13.3. Hazards 505

Inadvertent Ignition 505

Aging and Useful Life 506

Case Overpressure and Failure 506

Insensitive Munitions 508

Upper Pressure Limit 510

Toxicity 510

Safety Rules 510

13.4. Propellant Ingredients 511

Inorganic Oxidizers 513

Fuels 516

Binders 516

Burning-Rate Modifiers 517

Plasticizers 518

Curing Agents or Crosslinkers 518

Energetic Binders and Plasticizers 518

Organic Oxidizers or Explosives 518

Additives 519

Particle-Size Parameters 520

13.5. Other Propellant Categories 522

Gas Generator Propellants 522

Smokeless or Low-Smoke Propellant 523

Igniter Propellants 524

13.6. Liners, Insulators, and Inhibitors 525

13.7. Propellant Processing and Manufacture 528

Problems 531

References 534

14 Solid Propellant Combustion and Its Stability 536

14.1. Physical and Chemical Processes 536

14.2. Ignition Process 540

14.3. Extinction or Thrust Termination 541

14.4. Combustion Instability 543

Acoustic Instabilities 544

Analytical Models and Simulation of Combustion Stability 548

Combustion Stability Assessment, Remedy, and Design 548

Vortex-Shedding Instability 551

Problems 552

References 553

15 Solid Rocket Motor Components and Design 555

15.1. Rocket Motor Case 555

Metal Cases 559

Wound-Filament-Reinforced Plastic Cases 561

15.2. Nozzles 563

Classification 564

Design and Construction 566

Heat Absorption and Nozzle Materials 571

15.3. Igniter Hardware 577

Pyrotechnic Igniters 578

Pyrogen Igniters 579

Igniter Analysis and Design 581

15.4. Rocket Motor Design Approach 581

Problems 589

References 591

16 Hybrid Propellants Rocket Propulsion 593

16.1. Applications and Propellants 594

16.2. Interior Hybrid Motor Ballistics 599

16.3. Performance Analysis and Grain Configuration 602

Dynamic Behavior 605

16.4. Design Example 607

16.5. Combustion Instability 611

Symbols 615

Problems 617

References 618

17 Electric Propulsion 620

17.1. Ideal Flight Performance 626

17.2. Electrothermal Thrusters 631

Resistojets 631

Arcjets 634

17.3. Nonthermal Electrical Thrusters 638

Electrostatic Devices 638

Basic Relationships for Electrostatic Thrusters 640

Electromagnetic Thrusters 646

17.4. Optimum Flight Performance 654

17.5. Mission Applications 658

17.6. Electric Space-Power Supplies and Power-Conditioning Systems 661

Power Generation Units 661

Power-Conditioning Equipment (PCU or PPU) 664

Symbols 665

Problems 666

References 668

18 Thrust Vector Control 671

18.1. TVC Mechanisms with a Single Nozzle 673

18.2. TVC with Multiple Thrust Chambers or Nozzles 683

18.3. Testing 686

18.4. Integration with Vehicle 687

Problems 688

References 688

19 Selection of Rocket Propulsion Systems 690

19.1. Selection Process 692

19.2. Criteria for Selection 697

19.3. Interfaces 699

19.4. Cost Reduction 700

References 702

20 Rocket Exhaust Plumes 703

20.1. Plume Appearance and Flow Behavior 705

Spectral Distribution of Radiation 711

Multiple Nozzles 714

Plume Signature 714

Vehicle Base Geometry and Recirculation 715

Compression and Expansion Waves 716

20.2. Plume Effects 717

Smoke and Vapor Trails 717

Toxicity 718

Noise 719

Spacecraft Surface Contamination 720

Radio Signal Attenuation 720

Plume Impingement on Structures 722

Heat Transfer to Clusters of Liquid Propellant Rocket Engines 722

20.3. Analysis and Mathematical Simulation 723

Problems 724

References 724

21 Rocket Testing 726

21.1. Types of Tests 726

21.2. Test Facilities and Safeguards 728

Monitoring the Environment and Controlling Toxic Materials 731

21.3. Instrumentation and Data Management 735

Measurement System Terminology 736

Test Measurements 737

Health Monitoring System (HMS) 738

21.4. Flight Testing 739

21.5. Postaccident Procedures 740

References 741

Appendix 1 Conversion Factors and Constants 743

Conversion Factors (arranged alphabetically) 743

Constants 746

Appendix 2 Properties of the Earth's Standard Atmosphere 747

Appendix 3 Summary of Key equations for Ideal Chemical Rockets 749

Index 751

Additional information

CIN1118753658G
9781118753651
1118753658
Rocket Propulsion Elements by George P. Sutton (Massachusetts Institute of Technology Rocketdyne, a Division of Rockwell International Corporation)
Used - Good
Hardback
John Wiley & Sons Inc
20170207
800
N/A
Book picture is for illustrative purposes only, actual binding, cover or edition may vary.
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