LEADER 04810nam 2200613 a 450 001 9910792120503321 005 20230309003423.0 010 $a1-60086-567-4 010 $a1-60086-348-5 010 $a1-61583-527-X 035 $a(CKB)2590000000001141 035 $a(EBL)3111555 035 $a(OCoLC)922978816 035 $a(SSID)ssj0000403915 035 $a(PQKBManifestationID)12154338 035 $a(PQKBTitleCode)TC0000403915 035 $a(PQKBWorkID)10437888 035 $a(PQKB)10596156 035 $a(MiAaPQ)EBC3111555 035 $a(Au-PeEL)EBL3111555 035 $a(CaPaEBR)ebr10516659 035 $a(EXLCZ)992590000000001141 100 $a19840504d1984 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aFundamentals of solid-propellant combustion$b[electronic resource] /$fedited by Kenneth K. Kuo, Martin Summerfield 210 $aNew York, N.Y. $cAmerican Institute of Aeronautics and Astronautics, Inc.$dc1984 215 $a1 online resource (906 p.) 225 1 $aProgress in astronautics and aeronautics ;$vv. 90 300 $aDescription based upon print version of record. 311 $a0-915928-84-1 320 $aIncludes bibliographical references and index. 327 $aCover; 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 327 $aNitramine Composite PropellantsBurning 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 327 $aEffect of PressureEffect 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 327 $aPyrolysis of HMXShock 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 327 $aKinetics of HMX and RDX DecompositionProducts and Mechanism of HMX and RDX Pyrolysis; Catalysis of Nitramine Propellants; Flame Zone Chemistry; Chapter 5. Solid-Propellant Ignition Theories and Experiments; Introduction; Radiant Energy Ignition Sources; Shock Tube and Other Ignition Experiments; Theoretical Models of Solid-Propellant Ignition and Related Theory; Comments on Solution Methods; Solid-Phase Reaction Mechanism Theory; Theory of Ignition by Heterogeneous Reaction with External Oxidizer; Gas-Phase Theory of Solid-Propellant Ignition; Gas-Phase Theory-Shock Tube Cases 327 $aGas-Phase Theory-Radiant Heat Input 410 0$aProgress in astronautics and aeronautics ;$vv. 90. 606 $aSolid propellants$xCombustion 615 0$aSolid propellants$xCombustion. 676 $a629.1 s 701 $aKuo$b Kenneth K$013378 701 $aSummerfield$b Martin$021718 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910792120503321 996 $aFundamentals of solid-propellant combustion$93755964 997 $aUNINA