CONTENTS Duct Jet Propulsion / Rocket Propulsion / Applications of Rocket Propulsion / 15 References / 25
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1 CONTENTS PREFACE xi 1 Classification 1.1. Duct Jet Propulsion / Rocket Propulsion / Applications of Rocket Propulsion / 15 References / 25 2 Definitions and Fundamentals 2.1. Definition / Thrust / Exhaust Velocity / Energy and Efficiencies / Typical Performance Values / 39 Problems / 41 Symbols / 43 References / 44 3 Nozzle Theory and Thermodynamic Relations 3.1. Ideal Rocket / Summary of Thermodynamic Relations / Isentropic Flow through Nozzles /
2 vi CONTENTS 3.4. Nozzle Configurations / Real Nozzles / Four Performance Parameters / Nozzle Alignment / Variable Thrust / 96 Problems / 97 Symbols / 99 References / 100 Flight Performance 4.1. Gravity-Free Drag-Free Space Flight / Forces Acting on a Vehicle in the Atmosphere / Basic Relations of Motion / Effect of Propulsion System on Vehicle Performance / Space Flight / Flight Maneuvers / Flight Vehicles / Military Missiles / Aerodynamic Effect of Exhaust Plumes / Flight Stability / 153 Problems / 154 Symbols / 157 References / 159 Chemical Rocket Propellant Performance Analysis 5.1. Background and Fundamentals / Analysis of Chamber or Motor Case Conditions / Analysis of Nozzle Expansion Processes / Computer Analysis / Results of Thermochemical Calculations / 180 Problems / 189 Symbols / 193 References / 195 Liquid Propellant Rocket Engine Fundamentals 6.1. Propellants / Propellant Feed Systems / Gas Pressure Feed Systems /
3 CONTENTS vii 6.4. Propellant Tanks / Tank Pressurization / Turbopump Feed Systems and Engine Cycles / Flow and Pressure Balance / Rocket Engines for Maneuvering, Orbit Adjustments, or Attitude Control / Valves and Pipe Lines / Engine Support Structure / 235 Problems / 236 Symbols / 238 References / Liquid Propellants Propellant Properties / Liquid Oxidizers / Liquid Fuels / Liquid Monopropellants / Gelled Propellants / Gaseous Propellants / Safety and Environmental Concerns / 264 Problems / 265 Symbols / 266 References / Thrust Chambers Injectors / Combustion Chamber and Nozzle / Heat Transfer Analysis / Starting and Ignition / Variable Thrust / Sample Thrust Chamber Design Analysis / 324 Problems / 335 Symbols / 338 References / Combustion of Liquid Propellants Combustion Process / Analysis and Simulation / Combustion Instability / 348
4 VIII CONTENTS Problems / 360 References / Turbopumps, Engine Design, Engine Controls, Calibration, Integration, and Optimization Turbopumps / Performance of Complete or Multiple Rocket Propulsion Systems / Propellant Budget / Engine Design / Engine Controls / Engine System Calibration / System Integration and Engine Optimization / 411 Problems / 413 Symbols / 413 References / Solid Solid Propellant Rocket Fundamentals Propellant Burning Rate / 419 Basic Performance Relations / 437 Propellant Grain and Grain Configuration / 444 Propellant Grain Stress and Strain / 453 Attitude Control and Side Maneuvers with Solid Propellant Rocket Motors / 466 Problems / 467 Symbols / 470 References / 471 Propellants Classification / 474 Propellant Characteristics / 480 Hazards / 487 Propellant Ingredients / 494 Other Propellant Categories / 505 Liners, Insulators, and Inhibitors / 509 Propellant Processing and Manufacture / 511 Problems / 515 References /
5 CONTENTS ix 13 Combustion of Solid Propellants Physical and Chemical Processes / Ignition Process / Extinction or Thrust Termination / Combustion Instability / 528 Problems / 537 References / Solid Rocket Components and Motor Design Motor Case / Nozzle / Igniter Hardware / Rocket Motor Design Approach / 568 Problems / 575 References / Hybrid Propellant Rockets Applications and Propellants / Performance Analysis and Grain Configuration / Design Example / Combustion Instability / 599 Symbols / 604 References / Thrust Vector Control TVC Mechanisms with a Single Nozzle / TVC with Multiple Thrust Chambers or Nozzles / Testing / Integration with Vehicle / 621 References / Selection of Rocket Propulsion Systems Selection Process / Criteria for Selection / Interfaces / 634 References /
6 x CONTENTS 18 Rocket Exhaust Plumes Plume Appearance and Flow Behavior / 641 Plume Effects / 652 Analysis and Mathematical Simulation / 657 Problems / 658 References / Electric Propulsion Ideal Flight Performance / Electrothermal Thrusters / Non-Thermal Electric Thrusters / Optimum Flight Performance / Mission Applications / Electric Space-Power Supplies and Power-Conditioning Systems / 701 Problems / 706 Symbols / 707 References / Rocket Testing Types of Tests / Test Facilities and Safeguards / Instrumentation and Data Management / Flight Testing / Postaccident Procedures / 725 References / 726 Appendix 1 Appendix 2 Appendix 3 Appendix 4 Appendix 5 Index Conversion Factors and Constants Properties of the Earth's Standard Atmosphere Summary of Key Equations for Ideal Chemical Rockets Derivation of Hybrid Fuel Regression Rate Equation in Chapter 15 Alternative Interpretations of Boundary Layer Blowing Coefficient in Chapter
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