
Propellants and Explosives : Thermochemical Aspects of Combustion.
Title:
Propellants and Explosives : Thermochemical Aspects of Combustion.
Author:
Kubota, Naminosuke.
ISBN:
9783527693511
Personal Author:
Edition:
3rd ed.
Physical Description:
1 online resource (561 pages)
Contents:
Cover -- Title Page -- Copyright -- Contents -- Preface -- Preface to the Second Edition -- Preface to the First Edition -- Chapter 1 Foundations of Pyrodynamics -- 1.1 Heat and Pressure -- 1.1.1 First Law of Thermodynamics -- 1.1.2 Specific Heat -- 1.1.3 Entropy Change -- 1.2 Thermodynamics in a Flow Field -- 1.2.1 One-Dimensional Steady-State Flow -- 1.2.1.1 Sonic Velocity and Mach Number -- 1.2.1.2 Conservation Equations in a Flow Field -- 1.2.1.3 Stagnation Point -- 1.2.2 Formation of Shock Waves -- 1.2.3 Supersonic Nozzle Flow -- 1.3 Formation of Propulsive Forces -- 1.3.1 Momentum Change and Thrust -- 1.3.2 Rocket Propulsion -- 1.3.2.1 Thrust Coefficient -- 1.3.2.2 Characteristic Velocity -- 1.3.2.3 Specific Impulse -- 1.3.3 Gun Propulsion -- 1.3.3.1 Thermochemical Process of Gun Propulsion -- 1.3.3.2 Internal Ballistics -- 1.4 Formation of Destructive Forces -- 1.4.1 Pressure and Shock Wave -- 1.4.2 Shock Wave Propagation and Reflection in Solid Materials -- References -- Chapter 2 Thermochemistry of Combustion -- 2.1 Generation of Heat Energy -- 2.1.1 Chemical Bond Energy -- 2.1.2 Heat of Formation and Heat of Explosion -- 2.1.3 Thermal Equilibrium -- 2.2 Adiabatic Flame Temperature -- 2.3 Chemical Reaction -- 2.3.1 Thermal Dissociation -- 2.3.2 Reaction Rate -- 2.4 Evaluation of Chemical Energy -- 2.4.1 Heats of Formation of Reactants and Products -- 2.4.2 Oxygen Balance -- 2.4.3 Thermodynamic Energy -- References -- Chapter 3 Combustion Wave Propagation -- 3.1 Combustion Reactions -- 3.1.1 Ignition and Combustion -- 3.1.2 Premixed and Diffusion Flames -- 3.1.3 Laminar and Turbulent Flames -- 3.2 Combustion Wave of a Premixed Gas -- 3.2.1 Governing Equations for the Combustion Wave -- 3.2.2 Rankine-Hugoniot Relationships -- 3.2.3 Chapman-Jouguet Points -- 3.3 Structures of Combustion Waves.
3.3.1 Detonation Wave -- 3.3.2 Deflagration Wave -- 3.4 Ignition Reactions -- 3.4.1 The Ignition Process -- 3.4.2 Thermal Theory of Ignition -- 3.4.3 Flammability Limit -- 3.5 Combustion Waves of Energetic Materials -- 3.5.1 Thermal Theory of Burning Rate -- 3.5.1.1 Thermal Model of Combustion Wave Structure -- 3.5.1.2 Thermal Structure in the Condensed Phase -- 3.5.1.3 Thermal Structure in the Gas Phase -- 3.5.1.4 Burning Rate Model -- 3.5.2 Flame Stand-Off Distance -- 3.5.3 Burning Rate Characteristics of Energetic Materials -- 3.5.3.1 Pressure Exponent of Burning Rate -- 3.5.3.2 Temperature Sensitivity of Burning Rate -- 3.5.4 Analysis of Temperature Sensitivity of Burning Rate -- 3.5.5 Chemical Reaction Rate in Combustion Wave -- References -- Chapter 4 Energetics of Propellants and Explosives -- 4.1 Crystalline Materials -- 4.1.1 Physicochemical Properties of Crystalline Materials -- 4.1.2 Perchlorates -- 4.1.2.1 Ammonium Perchlorate -- 4.1.2.2 Nitronium Perchlorate -- 4.1.2.3 Potassium Perchlorate -- 4.1.3 Nitrates -- 4.1.3.1 Ammonium Nitrate -- 4.1.3.2 Potassium Nitrate and Sodium Nitrate -- 4.1.3.3 Pentaerythrol Tetranitrate -- 4.1.3.4 Triaminoguanidine Nitrate -- 4.1.4 Nitro Compounds -- 4.1.5 Nitramines -- 4.2 Polymeric Materials -- 4.2.1 Physicochemical Properties of Polymeric Materials -- 4.2.2 Nitrate Esters -- 4.2.3 Inert Polymers -- 4.2.4 Azide Polymers -- 4.2.4.1 GAP -- 4.2.4.2 BAMO -- 4.3 Classification of Propellants and Explosives -- 4.4 Formulation of Propellants -- 4.5 Nitropolymer Propellants -- 4.5.1 Single-Base Propellants -- 4.5.2 Double-Base Propellants -- 4.5.2.1 NC-NG Propellants -- 4.5.2.2 NC-TMETN Propellants -- 4.5.2.3 Nitro-Azide Polymer Propellants -- 4.5.2.4 Chemical Materials of Double-Base Propellants -- 4.6 Composite Propellants -- 4.6.1 AP Composite Propellants.
4.6.1.1 AP-HTPB Propellants -- 4.6.1.2 AP-GAP Propellants -- 4.6.1.3 Chemical Materials of AP Composite Propellants -- 4.6.2 AN Composite Propellants -- 4.6.3 Nitramine Composite Propellants -- 4.6.4 HNF Composite Propellants -- 4.6.5 TAGN Composite Propellants -- 4.7 Composite-Modified Double-Base Propellants -- 4.7.1 AP-CMDB Propellants -- 4.7.2 Nitramine CMDB Propellants -- 4.7.3 Triple-Base Propellants -- 4.8 Black Powder -- 4.9 Formulation of Explosives -- 4.9.1 Industrial Explosives -- 4.9.1.1 ANFO Explosives -- 4.9.1.2 Slurry Explosives -- 4.9.2 Military Explosives -- 4.9.2.1 TNT-Based Explosives -- 4.9.2.2 Plastic-Bonded Explosives -- References -- Chapter 5 Combustion of Crystalline and Polymeric Materials -- 5.1 Combustion of Crystalline Materials -- 5.1.1 Ammonium Perchlorate (AP) -- 5.1.1.1 Thermal Decomposition -- 5.1.1.2 Burning Rate -- 5.1.1.3 Combustion Wave Structure -- 5.1.2 Ammonium Nitrate (AN) -- 5.1.2.1 Thermal Decomposition -- 5.1.3 HMX -- 5.1.3.1 Thermal Decomposition -- 5.1.3.2 Burning Rate -- 5.1.3.3 Gas-Phase Reaction -- 5.1.3.4 Combustion Wave Structure and Heat Transfer -- 5.1.4 Triaminoguanidine Nitrate (TAGN) -- 5.1.4.1 Thermal Decomposition -- 5.1.4.2 Burning Rate -- 5.1.4.3 Combustion Wave Structure and Heat Transfer -- 5.1.5 ADN (Ammonium Dinitramide) -- 5.1.6 HNF (Hydrazinium Nitroformate) -- 5.2 Combustion of Polymeric Materials -- 5.2.1 Nitrate Esters -- 5.2.1.1 Decomposition of Methyl Nitrate -- 5.2.1.2 Decomposition of Ethyl Nitrate -- 5.2.1.3 Overall Decomposition Process of Nitrate Esters -- 5.2.1.4 Gas-Phase Reactions of NO_2 and NO -- 5.2.2 Glycidyl Azide Polymer (GAP) -- 5.2.2.1 Thermal Decomposition and Burning Rate -- 5.2.2.2 Combustion Wave Structure -- 5.2.3 Bis-azide Methyl Oxetane (BAMO) -- 5.2.3.1 Thermal Decomposition and Burning Rate.
5.2.3.2 Combustion Wave Structure and Heat Transfer -- References -- Chapter 6 Combustion of Double-Base Propellants -- 6.1 Combustion of NC-NG Propellants -- 6.1.1 Burning Rate Characteristics -- 6.1.2 Combustion Wave Structure -- 6.1.2.1 Gas-Phase Reaction Zones -- 6.1.2.2 A Simplified Reaction Model in Fizz Zone -- 6.1.3 Burning Rate Model -- 6.1.3.1 Model for Heat Feedback from the Gas Phase to the Condensed Phase -- 6.1.3.2 Burning Rate Calculated by a Simplified Gas-Phase Model -- 6.1.4 Energetics of the Gas Phase and Burning Rate -- 6.1.5 Temperature Sensitivity of Burning Rate -- 6.2 Combustion of NC-TMETN Propellants -- 6.2.1 Burning Rate Characteristics -- 6.2.2 Combustion Wave Structure -- 6.3 Combustion of Nitro-Azide Propellants -- 6.3.1 Burning Rate Characteristics -- 6.3.2 Combustion Wave Structure -- 6.4 Catalyzed Double-Base Propellants -- 6.4.1 Super-Rate, Plateau, and Mesa Burning -- 6.4.2 Effects of Lead Catalysts -- 6.4.2.1 Burning Rate Behavior of Catalyzed Liquid Nitrate Esters -- 6.4.2.2 Effect of Lead Compounds on Gas-Phase Reactions -- 6.4.3 Combustion of Catalyzed Double-Base Propellants -- 6.4.3.1 Burning Rate Characteristics -- 6.4.3.2 Reaction Mechanism in the Dark Zone -- 6.4.3.3 Reaction Mechanism in the Fizz Zone Structure -- 6.4.4 Combustion Models of Super-Rate, Plateau, and Mesa Burning -- 6.4.5 LiF-Catalyzed Double-Base Propellants -- 6.4.6 Ni-Catalyzed Double-Base Propellants -- 6.4.7 Suppression of Super-Rate and Plateau Burning -- References -- Chapter 7 Combustion of Composite Propellants -- 7.1 AP Composite Propellants -- 7.1.1 Combustion Wave Structure -- 7.1.1.1 Premixed Flame of AP Particles and Diffusion Flame -- 7.1.1.2 Burning Rate Model of Granular Diffusion Theory.
7.1.1.3 Combustion Wave Structure of Oxidizer-Rich AP Propellants -- 7.1.2 Burning Rate Characteristics -- 7.1.2.1 Effect of AP Particle Size -- 7.1.2.2 Effect of the Binder -- 7.1.2.3 Temperature Sensitivity -- 7.1.3 Catalyzed AP Composite Propellants -- 7.1.3.1 Positive Catalysts -- 7.1.3.2 LiF Negative Catalyst -- 7.1.3.3 SrCO_3 Negative Catalyst -- 7.2 Nitramine Composite Propellants -- 7.2.1 Burning Rate Characteristics -- 7.2.1.1 Effect of Nitramine Particle Size -- 7.2.1.2 Effect of Binder -- 7.2.2 Combustion Wave Structure -- 7.2.3 HMX-GAP Propellants -- 7.2.3.1 Physicochemical Properties of Propellants -- 7.2.3.2 Burning Rate and Combustion Wave Structure -- 7.2.4 Catalyzed Nitramine Composite Propellants -- 7.2.4.1 Super-Rate Burning of HMX Composite Propellants -- 7.2.4.2 Super-Rate Burning of HMX-GAP Propellants -- 7.2.4.3 LiF Catalysts for Super-Rate Burning -- 7.2.4.4 Catalyst Action of LiF on Combustion Wave -- 7.3 AP-Nitramine Composite Propellants -- 7.3.1 Theoretical Performance -- 7.3.2 Burning Rate -- 7.3.2.1 Effects of AP/RDX Mixture Ratio and Particle Size -- 7.3.2.2 Effect of Binder -- 7.4 TAGN-GAP Composite Propellants -- 7.4.1 Physicochemical Characteristics -- 7.4.2 Burning Rate and Combustion Wave Structure -- 7.5 AN-Azide Polymer Composite Propellants -- 7.5.1 AN-GAP Composite Propellants -- 7.5.2 AN-(BAMO-AMMO)-HMX Composite Propellants -- 7.6 AP-GAP Composite Propellants -- 7.7 ADN, HNF, and HNIW Composite Propellants -- References -- Chapter 8 Combustion of CMDB Propellants -- 8.1 Characteristics of CMDB Propellants -- 8.2 AP-CMDB Propellants -- 8.2.1 Flame Structure and Combustion Mode -- 8.2.2 Burning Rate Models -- 8.3 Nitramine-CMDB Propellants -- 8.3.1 Flame Structure and Combustion Mode -- 8.3.2 Burning Rate Characteristics -- 8.3.3 Thermal Wave Structure.
8.3.4 Burning Rate Model.
Abstract:
This third edition of the classic on the thermochemical aspects of the combustion of propellants and explosives is completely revised and updated and now includes a section on green propellants and offers an up-to-date view of the thermochemical aspects of combustion and corresponding applications. Clearly structured, the first half of the book presents an introduction to pyrodynamics, describing fundamental aspects of the combustion of energetic materials, while the second part highlights applications of energetic materials, such as propellants, explosives and pyrolants, with a focus on the phenomena occurring in rocket motors. Finally, an appendix gives a brief overview of the fundamentals of aerodynamics and heat transfer, which is a prerequisite for the study of pyrodynamics. A detailed reference for readers interested in rocketry or explosives technology.
Local Note:
Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2017. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
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