Addressing both experimental and theoretical aspects, this second edition of the classic covers the thermochemical and combustion characteristics of all important energetic materials. With five new chapters for updated coverage of significant developments plus two new appendices. Physikalisch-chemische Parameter wie Komponenten, Katalysatoren, Druck, Anfangstemperatur und Strömungsfeld bestimmen entscheidend das Abbrandverhalten von Treib- und Explosivstoffen. Das Buch beschreibt grundlegende Aspekte der thermochemischen Vorgänge bei der Zersetzung, Verbrennung, Deflagration und Detonation…mehr
Addressing both experimental and theoretical aspects, this second edition of the classic covers the thermochemical and combustion characteristics of all important energetic materials. With five new chapters for updated coverage of significant developments plus two new appendices.Physikalisch-chemische Parameter wie Komponenten, Katalysatoren, Druck, Anfangstemperatur und Strömungsfeld bestimmen entscheidend das Abbrandverhalten von Treib- und Explosivstoffen. Das Buch beschreibt grundlegende Aspekte der thermochemischen Vorgänge bei der Zersetzung, Verbrennung, Deflagration und Detonation von energetischen Materialien. Die Reaktionsmechanismen werden unter Berücksichtigung der Transportprozesse zwischen Verbrennungszone und Treibstoff diskutiert. Verbrennungsmodelle helfen die kontrollierenden Einflüsse von Druck und Anfangstemperatur auf die Regressionsrate und das Abbrandverhalten zu verstehen. Farbige Photographien unter hohem Druck brennender Treibstoffe zeigen die komplizierten Verbrennungsprozesse beim reaktiven Übergang von Flüssigkeit oder Feststoff in die Gasphase. Fortschrittliche Antriebssysteme wie luftatmende Triebwerke oder pyrotechnische Treibstoffe runden das Buch ab. Chemiker, Physiker, Materialwissenschaftler und Verfahrenstechniker in der wehrtechnischen und pyrotechnischen Industrie, in wehrtechnischen Ämtern sowie in Forschungsinstituten finden in diesem Buch einen ausführlichen und aktuellen Überblick über das Gebiet.
Dr. Naminosute Kubota received a Doctorate from Princeton University in 1973, majoring in 'Solid Propellant Combustion' and 'Rocket Propulsion including Ducted Rocket Engine'. His current position is Senior Research Scientist of Propellant Combustion Laboratory, Asahi Kasei Chemicals. Previously, he was Director, Third Research Center, Technical Research and Development Institute (TRDI), Japan Defense Agency, which is responsible for aircraft and missiles.
Inhaltsangabe
From the contents: Thermodynamics for energy conversion Fundamentals Thermodynamics in Flow Field Formation of Propulsive Forces Thermochemistry of combustion Generation of Heat Adiabatic Flame Temperature Chemical Reaction Combustion wave propagation Reaction for Combustion Combustion Wave of Premixed Gas Structure of Combustion Wave Reaction for Ignition Combustion Wave of Energetic Materials Energetics of Propellants and explosives Evaluation of Chemical Energy Crystalline and Polymeric Materials Classification of Propellants and Explosives Formulation of Propellants Nitropolymer Propellants Composite Propellants Formulation of Explosives Combustion of crystelline and polymeric materials
Combustion of Crystalline Materials Combustion of Polymeric Materials
Combustion of Double-base propellants NC-NG Propellants NC-TMETN Propellants Nitro-Azide Propellants Catalyzed Double-Base Propellants Combustion of composite Propellants AP Composite Propellants N itramine Composite Propellants TAGN Composite Propellants Composite Modified Double-Base Propellants Combution of explosives Detonation Velocity and Pressure Density and Detonation Velocity Applications of Detonation Phenomena Combustion in rocket motors Combustion Phenomena in Rocket Motor Ignition Transient Erosive Burning Wired propellant Burning; combustion Instability Ducted Rocket Engine Nomenclature Appendix IndexTHERMODYNAMICS FOR ENERGY CONVERSION Fundamentals Thermodynamics in Flow Field Formation of Propulsive Forces THERMOCHEMISTRY OF COMBUSTION Generation of Heat Adiabatic Flame Temperature Chemical Reaction COMBUSTION WAVE PROPAGATION Reaction for Combustion Combustion Wave of Premixed Gas Structure of Combustion Wave Reaction for Ignition Combustion Wave of Energetic Materials ENERGETICS OF PROPELLANTS AND EXPLOSIVES Evaluation of Chemical Energy Crystalline and Polymeric Materials Classification of Propellants and Explosives Formulation of Propellants Nitropolymer Propellants Composite Propellants Formulation of Explosives COMBUSTION OF CRYSTALLINE AND POLYMERIC MATERIALS Combustion of Crystalline Materials Combustion of Polymeric Materials COMBUSTION OF DOUBLE-BASE PROPELLANTS NC-NG Propellants NC-TMETN Propellants Nitro-Azide Propellants Catalyzed Double-Base Propellants COMBUSTION OF COMPOSITE PROPELLANTS AP Composite Propellants Nitramine Composite Propellants TAGN Composite Propellants Composite Modified Double-Base Propellants COMBUSTION OF EXPLOSIVES Detonation Velocity and Pressure Density and Detonation Velocity Applications of Detonation Phenomena COMBUSTION IN ROCKET MOTOR Combustion Phenomena in Rocket Motor Ignition Transient Erosive Burning Wired propellant Burning; combustion Instability Ducted Rocket Engine Nomenclature Appendix Index
From the contents: Thermodynamics for energy conversion Fundamentals Thermodynamics in Flow Field Formation of Propulsive Forces Thermochemistry of combustion Generation of Heat Adiabatic Flame Temperature Chemical Reaction Combustion wave propagation Reaction for Combustion Combustion Wave of Premixed Gas Structure of Combustion Wave Reaction for Ignition Combustion Wave of Energetic Materials Energetics of Propellants and explosives Evaluation of Chemical Energy Crystalline and Polymeric Materials Classification of Propellants and Explosives Formulation of Propellants Nitropolymer Propellants Composite Propellants Formulation of Explosives Combustion of crystelline and polymeric materials
Combustion of Crystalline Materials Combustion of Polymeric Materials
Combustion of Double-base propellants NC-NG Propellants NC-TMETN Propellants Nitro-Azide Propellants Catalyzed Double-Base Propellants Combustion of composite Propellants AP Composite Propellants N itramine Composite Propellants TAGN Composite Propellants Composite Modified Double-Base Propellants Combution of explosives Detonation Velocity and Pressure Density and Detonation Velocity Applications of Detonation Phenomena Combustion in rocket motors Combustion Phenomena in Rocket Motor Ignition Transient Erosive Burning Wired propellant Burning; combustion Instability Ducted Rocket Engine Nomenclature Appendix IndexTHERMODYNAMICS FOR ENERGY CONVERSION Fundamentals Thermodynamics in Flow Field Formation of Propulsive Forces THERMOCHEMISTRY OF COMBUSTION Generation of Heat Adiabatic Flame Temperature Chemical Reaction COMBUSTION WAVE PROPAGATION Reaction for Combustion Combustion Wave of Premixed Gas Structure of Combustion Wave Reaction for Ignition Combustion Wave of Energetic Materials ENERGETICS OF PROPELLANTS AND EXPLOSIVES Evaluation of Chemical Energy Crystalline and Polymeric Materials Classification of Propellants and Explosives Formulation of Propellants Nitropolymer Propellants Composite Propellants Formulation of Explosives COMBUSTION OF CRYSTALLINE AND POLYMERIC MATERIALS Combustion of Crystalline Materials Combustion of Polymeric Materials COMBUSTION OF DOUBLE-BASE PROPELLANTS NC-NG Propellants NC-TMETN Propellants Nitro-Azide Propellants Catalyzed Double-Base Propellants COMBUSTION OF COMPOSITE PROPELLANTS AP Composite Propellants Nitramine Composite Propellants TAGN Composite Propellants Composite Modified Double-Base Propellants COMBUSTION OF EXPLOSIVES Detonation Velocity and Pressure Density and Detonation Velocity Applications of Detonation Phenomena COMBUSTION IN ROCKET MOTOR Combustion Phenomena in Rocket Motor Ignition Transient Erosive Burning Wired propellant Burning; combustion Instability Ducted Rocket Engine Nomenclature Appendix Index
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