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Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield
| Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 |
| Descrizione fisica | 1 online resource (906 p.) |
| Disciplina | 629.1 s |
| Altri autori (Persone) |
KuoKenneth K
SummerfieldMartin |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Solid propellants - Combustion |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-567-4
1-60086-348-5 1-61583-527-X |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
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 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 Effect 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 Pyrolysis 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 Kinetics 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 Gas-Phase Theory-Radiant Heat Input |
| Record Nr. | UNINA-9910458920903321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield
| Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 |
| Descrizione fisica | 1 online resource (906 p.) |
| Disciplina | 629.1 s |
| Altri autori (Persone) |
KuoKenneth K
SummerfieldMartin |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Solid propellants - Combustion |
| ISBN |
1-60086-567-4
1-60086-348-5 1-61583-527-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
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 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 Effect 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 Pyrolysis 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 Kinetics 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 Gas-Phase Theory-Radiant Heat Input |
| Record Nr. | UNINA-9910792120503321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield
| Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 |
| Descrizione fisica | 1 online resource (906 p.) |
| Disciplina | 629.1 s |
| Altri autori (Persone) |
KuoKenneth K
SummerfieldMartin |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Solid propellants - Combustion |
| ISBN |
1-60086-567-4
1-60086-348-5 1-61583-527-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
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 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 Effect 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 Pyrolysis 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 Kinetics 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 Gas-Phase Theory-Radiant Heat Input |
| Record Nr. | UNINA-9910818063003321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Nonsteady burning and combustion stability of solid propellants [[electronic resource] /] / edited by Luigi De Luca, Edward W. Price, Martin Summerfield
| Nonsteady burning and combustion stability of solid propellants [[electronic resource] /] / edited by Luigi De Luca, Edward W. Price, Martin Summerfield |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, 1992 |
| Descrizione fisica | 1 online resource (895 p.) |
| Altri autori (Persone) |
De LucaLuigi
PriceEdward W SummerfieldMartin |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Solid propellants - Combustion |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-615-8
1-60086-396-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Chapter 1. Solid Rocket Combustion Instability�An American Historical Accoun""; ""Chapter 2. Introduction to Nonsteady Burning and Combustion Stability""; ""Chapter 3. Steady Burning Rate and Affecting Factors:Experimental Results""; ""Chapter 4. Temperature Sensitivity of Solid Propellants and Affecting Factors:Experimental Results""; ""Chapter 5. Measuring Thermodynamic Properties of Burning Propellants""; ""Chapter 6. Thermophysics of Stable Combustion Waves of Solid Propellants""
""Chapter 7. Flame Structure of Modern Solid Propellants""""Chapter 8. Nonintrusive Diagnostic Techniques for Research on Nonsteady Burning of Solid Propellants""; ""Chapter 9. L* Instability""; ""Chapter 10. Radiation-Driven Transient Burning: Experimental Results""; ""Chapter 11. Self-Sustained Oscillatory Burning of Solid Propellants: Experimental Results""; ""Chapter 12. Transient Combustion of Solid Propellants: An Important Aspect of Deflagration-to-Detonation Transition""; ""Chapter 13. Coupling Between Nonsteady Burning and Structural Mechanics of Solid-Propellant Grains"" ""Chapter 14. Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by Flame Models""""Chapter 15. Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by the Zeldovich-Novozhilov Method""; ""Chapter 16. Numerical Computations of Solid-Propellant Nonsteady Burning in Open or Confined Volumes""; ""Chapter 17. Laboratory Test Methods for Combustion-Stability Properties of Solid Propellants""; ""Chapter 18. Prediction of the Stability of Unsteady Motions in Solid-Propellant Rocket Motors"" ""Chapter 19. Applications of Combustion-Stability Technology to Solid-Propellant Rocket Motors""""Chapter 20. Technologies and Techniques for Instability Suppression in Motors""; ""Chapter 21. Status and Prospects for Future Developments""; ""Author Index"" |
| Record Nr. | UNINA-9910457202003321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Nonsteady burning and combustion stability of solid propellants [[electronic resource] /] / edited by Luigi De Luca, Edward W. Price, Martin Summerfield
| Nonsteady burning and combustion stability of solid propellants [[electronic resource] /] / edited by Luigi De Luca, Edward W. Price, Martin Summerfield |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, 1992 |
| Descrizione fisica | 1 online resource (895 p.) |
| Altri autori (Persone) |
De LucaLuigi
PriceEdward W SummerfieldMartin |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Solid propellants - Combustion |
| ISBN |
1-60086-615-8
1-60086-396-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Chapter 1. Solid Rocket Combustion Instability�An American Historical Accoun""; ""Chapter 2. Introduction to Nonsteady Burning and Combustion Stability""; ""Chapter 3. Steady Burning Rate and Affecting Factors:Experimental Results""; ""Chapter 4. Temperature Sensitivity of Solid Propellants and Affecting Factors:Experimental Results""; ""Chapter 5. Measuring Thermodynamic Properties of Burning Propellants""; ""Chapter 6. Thermophysics of Stable Combustion Waves of Solid Propellants""
""Chapter 7. Flame Structure of Modern Solid Propellants""""Chapter 8. Nonintrusive Diagnostic Techniques for Research on Nonsteady Burning of Solid Propellants""; ""Chapter 9. L* Instability""; ""Chapter 10. Radiation-Driven Transient Burning: Experimental Results""; ""Chapter 11. Self-Sustained Oscillatory Burning of Solid Propellants: Experimental Results""; ""Chapter 12. Transient Combustion of Solid Propellants: An Important Aspect of Deflagration-to-Detonation Transition""; ""Chapter 13. Coupling Between Nonsteady Burning and Structural Mechanics of Solid-Propellant Grains"" ""Chapter 14. Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by Flame Models""""Chapter 15. Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by the Zeldovich-Novozhilov Method""; ""Chapter 16. Numerical Computations of Solid-Propellant Nonsteady Burning in Open or Confined Volumes""; ""Chapter 17. Laboratory Test Methods for Combustion-Stability Properties of Solid Propellants""; ""Chapter 18. Prediction of the Stability of Unsteady Motions in Solid-Propellant Rocket Motors"" ""Chapter 19. Applications of Combustion-Stability Technology to Solid-Propellant Rocket Motors""""Chapter 20. Technologies and Techniques for Instability Suppression in Motors""; ""Chapter 21. Status and Prospects for Future Developments""; ""Author Index"" |
| Record Nr. | UNINA-9910781700003321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Nonsteady burning and combustion stability of solid propellants [[electronic resource] /] / edited by Luigi De Luca, Edward W. Price, Martin Summerfield
| Nonsteady burning and combustion stability of solid propellants [[electronic resource] /] / edited by Luigi De Luca, Edward W. Price, Martin Summerfield |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, 1992 |
| Descrizione fisica | 1 online resource (895 p.) |
| Altri autori (Persone) |
De LucaLuigi
PriceEdward W SummerfieldMartin |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Solid propellants - Combustion |
| ISBN |
1-60086-615-8
1-60086-396-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Chapter 1. Solid Rocket Combustion Instability�An American Historical Accoun""; ""Chapter 2. Introduction to Nonsteady Burning and Combustion Stability""; ""Chapter 3. Steady Burning Rate and Affecting Factors:Experimental Results""; ""Chapter 4. Temperature Sensitivity of Solid Propellants and Affecting Factors:Experimental Results""; ""Chapter 5. Measuring Thermodynamic Properties of Burning Propellants""; ""Chapter 6. Thermophysics of Stable Combustion Waves of Solid Propellants""
""Chapter 7. Flame Structure of Modern Solid Propellants""""Chapter 8. Nonintrusive Diagnostic Techniques for Research on Nonsteady Burning of Solid Propellants""; ""Chapter 9. L* Instability""; ""Chapter 10. Radiation-Driven Transient Burning: Experimental Results""; ""Chapter 11. Self-Sustained Oscillatory Burning of Solid Propellants: Experimental Results""; ""Chapter 12. Transient Combustion of Solid Propellants: An Important Aspect of Deflagration-to-Detonation Transition""; ""Chapter 13. Coupling Between Nonsteady Burning and Structural Mechanics of Solid-Propellant Grains"" ""Chapter 14. Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by Flame Models""""Chapter 15. Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by the Zeldovich-Novozhilov Method""; ""Chapter 16. Numerical Computations of Solid-Propellant Nonsteady Burning in Open or Confined Volumes""; ""Chapter 17. Laboratory Test Methods for Combustion-Stability Properties of Solid Propellants""; ""Chapter 18. Prediction of the Stability of Unsteady Motions in Solid-Propellant Rocket Motors"" ""Chapter 19. Applications of Combustion-Stability Technology to Solid-Propellant Rocket Motors""""Chapter 20. Technologies and Techniques for Instability Suppression in Motors""; ""Chapter 21. Status and Prospects for Future Developments""; ""Author Index"" |
| Record Nr. | UNINA-9910812548103321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Solid propellant rocket research [[electronic resource] /] / edited by Martin Summerfield
| Solid propellant rocket research [[electronic resource] /] / edited by Martin Summerfield |
| Pubbl/distr/stampa | New York, : Academic Press, 1960 |
| Descrizione fisica | 1 online resource (712 p.) |
| Disciplina | 629.134354 |
| Altri autori (Persone) | SummerfieldMartin |
| Collana | Progress in astronautics and rocketry |
| Soggetto topico | Solid propellant rockets |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-476-7
1-60086-257-8 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Solid Rockets Committee and Symposium Papers Committee""; ""Contributors to Volume 1""; ""Preface to the Series""; ""Preface to the Volume""; ""Contents""; ""A. Mechanical Properties of Grains""; ""Grain Design and Development Problems for Very Large Rocket Motors""; ""On ""Poisson's Ratio"" in Linear Visco-Elastic Propellants""; ""Mechanical Properties and the Design of Solid Propellant Motors""; ""A Method of Strength Analysis of Solid Propellant Rocket Grains""; ""Stress and Strain Analysis of Cylindrical Case-Bonded Grains""
""B. Steady-State Burning Mechanisms""""Burning Mechanism of Ammonium Perchlorate Propellants""; ""Some Research Problems in the Steady-State Burning of Composite Solid Propellants""; ""A Theoretical Study of the Burning of a Solid Propellant Sandwich""; ""The Role of Binder in Composite Propellant Combustion""; ""C. Combustion of Metals""; ""Combustion of Metals: Physical Considerations""; ""The Experimental Nature of the Combustion of Metallic Powders""; ""Combustion Characteristics of Metal Particles""; ""The Combustion of Elemental Boron""; ""Metal Combustion in Deflagrating Propellant"" ""D. Theories of Unstable Combustion""""Solid Propellant Rocket Motors as Acoustic Oscillators""; ""Heat Transfer Stability Analysis of Solid Propellant Rocket Motors""; ""A Theory of Oscillatory Burning of Solid Propellants Assuming a Constant Surface Temperature""; ""Combustion Instability in Solid Rockets Using Propellants with Reactive Additives""; ""The Influence of Erosive Burning on Acoustic Instability in Solid Propellant Rocket Motors""; ""E. Experiments on Unstable Burning""; ""An Experimental Investigation of Unstable Combustion in Solid propellant Rocket Motors"" ""Experimental Investigations of Unstable Burning in Solid Propellant Rocket Motors""""Unstable Burning Phenomenon in Double-Base Propellants""; ""Review of Experimental Research on Combustion Instability of Solid Propellants""; ""Resonant Burning of Solid Propellants: Review of Causes, Cures and Effects""; ""F. Solid Propellant Ignition""; ""The Mechanism of Ignition of Composite Solid Propellants by Hot Gases""; ""Propellant Ignition by High Convective Heat Fluxes""; ""Solid Propellant Ignition Studies With High Flux Radiant Energy as a Thermal Source"" |
| Record Nr. | UNINA-9910457209903321 |
| New York, : Academic Press, 1960 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Solid propellant rocket research [[electronic resource] /] / edited by Martin Summerfield
| Solid propellant rocket research [[electronic resource] /] / edited by Martin Summerfield |
| Pubbl/distr/stampa | New York, : Academic Press, 1960 |
| Descrizione fisica | 1 online resource (712 p.) |
| Disciplina | 629.134354 |
| Altri autori (Persone) | SummerfieldMartin |
| Collana | Progress in astronautics and rocketry |
| Soggetto topico | Solid propellant rockets |
| ISBN |
1-60086-476-7
1-60086-257-8 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Solid Rockets Committee and Symposium Papers Committee""; ""Contributors to Volume 1""; ""Preface to the Series""; ""Preface to the Volume""; ""Contents""; ""A. Mechanical Properties of Grains""; ""Grain Design and Development Problems for Very Large Rocket Motors""; ""On ""Poisson's Ratio"" in Linear Visco-Elastic Propellants""; ""Mechanical Properties and the Design of Solid Propellant Motors""; ""A Method of Strength Analysis of Solid Propellant Rocket Grains""; ""Stress and Strain Analysis of Cylindrical Case-Bonded Grains""
""B. Steady-State Burning Mechanisms""""Burning Mechanism of Ammonium Perchlorate Propellants""; ""Some Research Problems in the Steady-State Burning of Composite Solid Propellants""; ""A Theoretical Study of the Burning of a Solid Propellant Sandwich""; ""The Role of Binder in Composite Propellant Combustion""; ""C. Combustion of Metals""; ""Combustion of Metals: Physical Considerations""; ""The Experimental Nature of the Combustion of Metallic Powders""; ""Combustion Characteristics of Metal Particles""; ""The Combustion of Elemental Boron""; ""Metal Combustion in Deflagrating Propellant"" ""D. Theories of Unstable Combustion""""Solid Propellant Rocket Motors as Acoustic Oscillators""; ""Heat Transfer Stability Analysis of Solid Propellant Rocket Motors""; ""A Theory of Oscillatory Burning of Solid Propellants Assuming a Constant Surface Temperature""; ""Combustion Instability in Solid Rockets Using Propellants with Reactive Additives""; ""The Influence of Erosive Burning on Acoustic Instability in Solid Propellant Rocket Motors""; ""E. Experiments on Unstable Burning""; ""An Experimental Investigation of Unstable Combustion in Solid propellant Rocket Motors"" ""Experimental Investigations of Unstable Burning in Solid Propellant Rocket Motors""""Unstable Burning Phenomenon in Double-Base Propellants""; ""Review of Experimental Research on Combustion Instability of Solid Propellants""; ""Resonant Burning of Solid Propellants: Review of Causes, Cures and Effects""; ""F. Solid Propellant Ignition""; ""The Mechanism of Ignition of Composite Solid Propellants by Hot Gases""; ""Propellant Ignition by High Convective Heat Fluxes""; ""Solid Propellant Ignition Studies With High Flux Radiant Energy as a Thermal Source"" |
| Record Nr. | UNINA-9910781699403321 |
| New York, : Academic Press, 1960 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Solid propellant rocket research [[electronic resource] /] / edited by Martin Summerfield
| Solid propellant rocket research [[electronic resource] /] / edited by Martin Summerfield |
| Pubbl/distr/stampa | New York, : Academic Press, 1960 |
| Descrizione fisica | 1 online resource (712 p.) |
| Disciplina | 629.134354 |
| Altri autori (Persone) | SummerfieldMartin |
| Collana | Progress in astronautics and rocketry |
| Soggetto topico | Solid propellant rockets |
| ISBN |
1-60086-476-7
1-60086-257-8 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Solid Rockets Committee and Symposium Papers Committee""; ""Contributors to Volume 1""; ""Preface to the Series""; ""Preface to the Volume""; ""Contents""; ""A. Mechanical Properties of Grains""; ""Grain Design and Development Problems for Very Large Rocket Motors""; ""On ""Poisson's Ratio"" in Linear Visco-Elastic Propellants""; ""Mechanical Properties and the Design of Solid Propellant Motors""; ""A Method of Strength Analysis of Solid Propellant Rocket Grains""; ""Stress and Strain Analysis of Cylindrical Case-Bonded Grains""
""B. Steady-State Burning Mechanisms""""Burning Mechanism of Ammonium Perchlorate Propellants""; ""Some Research Problems in the Steady-State Burning of Composite Solid Propellants""; ""A Theoretical Study of the Burning of a Solid Propellant Sandwich""; ""The Role of Binder in Composite Propellant Combustion""; ""C. Combustion of Metals""; ""Combustion of Metals: Physical Considerations""; ""The Experimental Nature of the Combustion of Metallic Powders""; ""Combustion Characteristics of Metal Particles""; ""The Combustion of Elemental Boron""; ""Metal Combustion in Deflagrating Propellant"" ""D. Theories of Unstable Combustion""""Solid Propellant Rocket Motors as Acoustic Oscillators""; ""Heat Transfer Stability Analysis of Solid Propellant Rocket Motors""; ""A Theory of Oscillatory Burning of Solid Propellants Assuming a Constant Surface Temperature""; ""Combustion Instability in Solid Rockets Using Propellants with Reactive Additives""; ""The Influence of Erosive Burning on Acoustic Instability in Solid Propellant Rocket Motors""; ""E. Experiments on Unstable Burning""; ""An Experimental Investigation of Unstable Combustion in Solid propellant Rocket Motors"" ""Experimental Investigations of Unstable Burning in Solid Propellant Rocket Motors""""Unstable Burning Phenomenon in Double-Base Propellants""; ""Review of Experimental Research on Combustion Instability of Solid Propellants""; ""Resonant Burning of Solid Propellants: Review of Causes, Cures and Effects""; ""F. Solid Propellant Ignition""; ""The Mechanism of Ignition of Composite Solid Propellants by Hot Gases""; ""Propellant Ignition by High Convective Heat Fluxes""; ""Solid Propellant Ignition Studies With High Flux Radiant Energy as a Thermal Source"" |
| Record Nr. | UNINA-9910811645003321 |
| New York, : Academic Press, 1960 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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