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Vigor Yang, Pennsylvania State University
Thomas B. Brill, University of Delaware
Wu-Zhen Ren, China Ordnance Industry Ministry
Progress in Astronautics and Aeronautics Series, V-185
Published by AIAA, © 2000, 990 pages, Hardback
ISBN-10: 1-56347-442-5
ISBN-13: 978-1-56347-442-2
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AIAA Member Price:
$94.95
List Price:
$124.95
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This volume brings together the world’s most highly regarded scientists in the field of solid rocket propulsion. Thirty-nine papers present in-depth coverage on a wide range of topics including: advanced materials and nontraditional formulations; the chemical aspects of organic and inorganic components in relation to decomposition mechanisms, kinetics, combustion, and modeling; safety issues, hazards and explosive characteristics; and experimental and computational interior ballistics research, including chemical information and the physics of the complex flowfield.
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Table of Contents:
- Part I. Propellant Chemistry, Synthesis, and Formulation
- Flash Pyrolysis of Ammonium Perchlorate–Hydroxly-Terminated Polybutadiene Mixtures Including Selected Additives
- Gas Phase Chemical Kinetics of [C,H,N,O] Systems Relevant to the Combustion of Nitramines
- Reactivity of Azide Polymer Propellants
- Effect of Molecular Structure on Combustion of Polynitrogen Energetic Materials
- Molecular Structure Tailoring of Binders in Solid Propellants
- Effects of Microstructure on Explosive Behavior
- Advances in Solid Propellant Formulations
- Synthesis and Characterization of Dinitramidic Acid and Its Salts
- Hazards Associated with Solid Propellants
- Part II. Combustion of Solid Energetic Materials
- Overview of Combustion Mechanisms and Flame Structures for Advanced Solid Propellants
- Physico-Chemical Mechanisms of Solid Propellant Combustion
- Flame Structure of Solid Propellants
- Experimental Studies of Nitramine/Azide Propellant Combustion
- Optical Diagnostics of Solid-Propellant Flame Structures
- Thermal Decomposition and Combustion of GAP/AN/Nitrate Ester Propellants
- Thermal Decomposition of Potassium Dinitramide at Elevated Pressure
- Combustion Mechanisms of 3-Azidomethyl-3-Methyloxetane (AMMO) Composite Propellants
- Burning Rate Characteristics of Glycidly Azide Polymer (GAP) Fuels and Propellants
- Effects of Carbon Substances on Combustion Properties of Catalyzed RDX-CMDB Propellants
- Modeling of RDX/GAP Propellant Combustion with Detailed Chemical Kinetics
- Energetic-Material Combustion Modeling with Elementary Gas-Phase Reactions: A Practical Approach
- Burning Rate Prediction of Double Base Plateau Propellants
- Structure and Stability of Deflagrations in Porous Energetic Materials
- Modeling of Cook-Off Reaction Violence of Confined Energetic Materials
- Solid Propellant Combustion Response: Quasi-Steady (QSHOD) Theory Development and Validation
- Burning-Rate Response Functions of Composite-Modified Double Base Propellants and HMX
- Combustion of Aluminized Solid Propellants
- Detailed Studies on the Flame Structure of Aluminum Particle Combustion
- Combustion of Aluminum Particles in Solid Rocket Motor Flows
- Formation of Condensed Combustion Products at the Burning Surface of Solid Rocket Propellant
- Measurements of the Physico-Chemical Properties of Liquid Alumina Using Contactless Techniques
- Part III. Motor Interior Ballistics
- Effect of Acoustic Oscillation on Flow Development in a Simulated Nozzleless Rocket Motor
- Stability and Acoustic Resonance of Internal Flows Generated by Side Injection
- Turbulent Transport in Rocket Motor Unsteady Flowfield
- Some Aspects of Two-Phase Flows in Solid-Propellant Rocket Motors
- Combustion Dynamics of Homogeneous Solid Propellants in a Rocket Motor with Acoustic Excitations
- Combustion Characteristics of Aluminized HTPB/AP Propellant in Acceleration Fields
- Pulsed Motor Firings
- Transverse Waves in Solid- Propellant Rocket Motors: Pulse-Triggered Unstable Mode
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