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Fundamentals of Solid-Propellant Combustion.

Author: Kenneth K Kuo; Martin Summerfield
Publisher: Reston : American Institute of Aeronautics and Astronautics, 2000.
Series: Progress in astronautics and aeronautics.
Edition/Format:   eBook : Document : EnglishView all editions and formats
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Genre/Form: Electronic books
Additional Physical Format: Print version:
Kuo, Kenneth K.
Fundamentals of Solid-Propellant Combustion.
Reston : American Institute of Aeronautics and Astronautics, ©2000
Material Type: Document, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: Kenneth K Kuo; Martin Summerfield
ISBN: 9781600863486 1600863485
OCLC Number: 922978816
Notes: ""Radiant Energy Ignition Sources""
Description: 1 online resource (906 pages).
Contents: ""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Authors""; ""Preface""; ""Acknowledgments""; ""Chapter 1. Survey of Rocket Propellants and Their Combustion Characteristics""; ""Performance of a Solid-Propellant Rocket Motor""; ""Stable Combustion of a Rocket Motor""; ""Temperature Sensitivity of Burning Rate""; ""Thermochemical Properties of Propellant Ingredients""; ""Thermochemical Properties of Propellant Combustion Products""; ""Combustion Processes of Various Types of Solid Propellants""; ""Double-Base Propellants""; ""Ammonium Perchlorate Composite Propellants"" ""Composite Modified Double-Base Propellants""""Nitramine Composite Propellants""; ""Burning Rate Controlling Factors of Solid Propellants""; ""Combustion Characteristics Required for Solid Propellants and General Description of the Combustion Wave""; ""Heat-Transfer Mechanism in Combustion Waves""; ""Heat Transfer in Solid Phase""; ""Heat Transfer in Gas Phase""; ""Reaction Rate in Gas Phase""; ""Burning Rate of Solid Propellant Calculated by a Simplified Gas-Phase Model""; ""Chapter 2. Chemistry of Ignition and Combustion of Ammonium-Perchlorate-Based Propellants"" ""Chemistry of Ignition""""Sequence of Ignition""; ""Theories of Ignition""; ""Role of Oxidizer and Binder""; ""Effect of Pressure""; ""Effect of Oxidizing Atmosphere""; ""Ignition of Composite Propellant Fuels by HClO(sub[4]) Vapor""; ""Preignition Reactions""; ""Effect of Catalysts on Ignition""; ""Chemistry of Combustion""; ""Introduction to Combustion Mechanism""; ""Surface Reactions""; ""Subsurface Reactions""; ""Gas-Phase Reactions""; ""Effect of Catalysts on Propellant Combustion""; ""Future Research Directions"" ""Chapter 3. The Thermal Behavior of Cyclotrimethylenetrinitramine (RDX) and Cyclotetramethylenetetranitramine (HMX)""""Crystallography""; ""Sublimation of HMX""; ""Decomposition of the Solid RDX and HMX""; ""Liquefaction""; ""Decomposition of Liquid""; ""Pyrolysis of HMX""; ""Shock Tube Studies""; ""Ignition of HMX""; ""Self-Deflagration of HMX and RDX""; ""Self-Deflagration Rate as a Function of Pressure""; ""Self-Deflagration Rate as a Function of Pressure and Initial Sample Temperature""; ""Surface Structure of Self-Deflagrating HMX"" ""Chapter 4. Chemistry of Nitrate Ester and Nitramine Propellants""""Decomposition of Nitrocellulose""; ""Kinetics of Nitrocellulose Decomposition""; ""Products and Mechanism of Nitrocellulose Decomposition""; ""Plasticizers and Stabilizers in Nitrocellulose Decomposition""; ""Catalysis of Nitrate Ester Propellants""; ""Decomposition of Nitramines""; ""Kinetics of HMX and RDX Decomposition""; ""Products and Mechanism of HMX and RDX Pyrolysis""; ""Catalysis of Nitramine Propellants""; ""Flame Zone Chemistry""; ""Chapter 5. Solid-Propellant Ignition Theories and Experiments""; ""Introduction""
Series Title: Progress in astronautics and aeronautics.

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