Description

Book Synopsis
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.

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

Rocket Propulsion Elements

    Product form

    £114.26

    Includes FREE delivery

    RRP £126.95 – you save £12.69 (9%)

    Order before 4pm today for delivery by Fri 19 Jun 2026.

    A Hardback by George P. Sutton, Oscar Biblarz

    1 in stock

      Trusted by thousands of customers. See 2,385+ Customer Reviews

      View other formats and editions of Rocket Propulsion Elements by George P. Sutton

      Publisher: John Wiley & Sons Inc
      Publication Date: 07/02/2017
      ISBN13: 9781118753651, 978-1118753651
      ISBN10: 1118753658

      Description

      Book Synopsis
      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.

      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

      Recently viewed products

      © 2026 Book Curl

        • American Express
        • Apple Pay
        • Diners Club
        • Discover
        • Google Pay
        • Maestro
        • Mastercard
        • PayPal
        • Shop Pay
        • Union Pay
        • Visa

        Login

        Forgot your password?

        Don't have an account yet?
        Create account