01498nam 2200481 450 991082192190332120230808193311.080-246-3246-2(CKB)3710000000686114(EBL)4543685(MiAaPQ)EBC4543685(Au-PeEL)EBL4543685(CaPaEBR)ebr11232041(OCoLC)953658682(EXLCZ)99371000000068611420160714h20162016 uy 0czeur|n|---|||||rdacontentrdamediardacarrierMolekularni genetika pro bioanalytiky /Martin Beranek1. vydani.Praha, [Czech Republic] :Nakladatelstvi Karolinum,2016.©20161 online resource (194 p.)Ucebni Texty Univerzity Karlovy V PrazeDescription based upon print version of record.80-246-3224-1 Includes bibliographical references at the end of each chapters.8.6 Klinický význam molekulárního klonováníUčební texty Univerzity Karlovy v Praze.Molecular geneticsMolecular genetics.574.87328Beranek Martin1637255MiAaPQMiAaPQMiAaPQBOOK9910821921903321Molekularni genetika pro bioanalytiky3978986UNINA04810nam 2200613 a 450 991081806300332120230309003423.01-60086-567-41-60086-348-51-61583-527-X(CKB)2590000000001141(EBL)3111555(OCoLC)922978816(SSID)ssj0000403915(PQKBManifestationID)12154338(PQKBTitleCode)TC0000403915(PQKBWorkID)10437888(PQKB)10596156(MiAaPQ)EBC3111555(Au-PeEL)EBL3111555(CaPaEBR)ebr10516659(EXLCZ)99259000000000114119840504d1984 uy 0engur|n|---|||||txtccrFundamentals of solid-propellant combustion[electronic resource] /edited by Kenneth K. Kuo, Martin SummerfieldNew York, N.Y. American Institute of Aeronautics and Astronautics, Inc.c19841 online resource (906 p.)Progress in astronautics and aeronautics ;v. 90Description based upon print version of record.0-915928-84-1 Includes bibliographical references and index.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 PropellantsNitramine 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 BinderEffect 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 LiquidPyrolysis 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 NitraminesKinetics 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 CasesGas-Phase Theory-Radiant Heat InputProgress in astronautics and aeronautics ;v. 90.Solid propellantsCombustionSolid propellantsCombustion.629.1 sKuo Kenneth K13378Summerfield Martin21718MiAaPQMiAaPQMiAaPQBOOK9910818063003321Fundamentals of solid-propellant combustion4112096UNINA01447nam0 22002893i 450 VAN010366920180220105005.228978-02-992297-0-220151120d2009 |0itac50 baengUS|||| |||||Nox philologiaeAulus Gellius and the fantasy of the Roman libraryErik GundersonMadison : University of Wisconsin press, 2009IX313 p. ; 24 cmNella p. contro il frontespizio: publication of this volume has been made possible in part through the generous support and enduring vision of Warren G. Moon.001VAN00016142001 Wisconsin studies in classics210 [Madison]University of WisconsinBristolBristol.MadisonVANL000130GundersonErikVANV080860515594University of Wisconsin <editore>VANV108489650ITSOL20240503RICAhttps://books.google.it/books?id=T1JnvNucVBkC&printsec=frontcover&hl=ithttps://books.google.it/books?id=T1JnvNucVBkC&printsec=frontcover&hl=itBIBLIOTECA DEL DIPARTIMENTO DI LETTERE E BENI CULTURALIIT-CE0103VAN07VAN0103669BIBLIOTECA DEL DIPARTIMENTO DI LETTERE E BENI CULTURALI07CONS Fa 911 07UBL251 20151120 Nox philologiae1410369UNICAMPANIA