Info
- Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.
Electrothermal-chemical (ETC) closed-chamber interrupted-burning tests with JA2 and M30 solid propellants [[electronic resource] /] / Avi Birk ... [and others]
| Electrothermal-chemical (ETC) closed-chamber interrupted-burning tests with JA2 and M30 solid propellants [[electronic resource] /] / Avi Birk ... [and others] |
| Pubbl/distr/stampa | Aberdeen Proving Ground, MD : b U.S. Army Research Laboratory, : [publisher not identified], , [2000] |
| Descrizione fisica | 1 online resource (viii, 30 pages) : illustrations |
| Altri autori (Persone) | BirkAvi |
| Collana | ARL-TR |
| Soggetto topico |
Solid propellants - Combustion
Solid propellants - Thermal properties Explosives, Military Thermochemistry |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Electrothermal-chemical |
| Record Nr. | UNINA-9910699695003321 |
| Aberdeen Proving Ground, MD : b U.S. Army Research Laboratory, : [publisher not identified], , [2000] | ||
| 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 |
| 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 | ||
| ||
The observed nature of ignition and burning of two solid propellants at pressures below one atmosphere / / T.G. Lee
| The observed nature of ignition and burning of two solid propellants at pressures below one atmosphere / / T.G. Lee |
| Autore | Lee T. G |
| Pubbl/distr/stampa | Gaithersburg, MD : , : U.S. Dept. of Commerce, National Institute of Standards and Technology, , 1957 |
| Descrizione fisica | 1 online resource |
| Altri autori (Persone) | LeeT. G |
| Collana | NBS report |
| Soggetto topico | Solid propellants - Combustion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910711112403321 |
Lee T. G
|
||
| Gaithersburg, MD : , : U.S. Dept. of Commerce, National Institute of Standards and Technology, , 1957 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Self-heating characteristics of a solid propellant / / Joseph Loftus
| Self-heating characteristics of a solid propellant / / Joseph Loftus |
| Autore | Loftus Joseph |
| Pubbl/distr/stampa | Gaithersburg, MD : , : U.S. Dept. of Commerce, National Institute of Standards and Technology, , 1957 |
| Descrizione fisica | 1 online resource |
| Altri autori (Persone) | LoftusJoseph |
| Collana | NBS report |
| Soggetto topico | Solid propellants - Combustion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910711293703321 |
|
Loftus Joseph
|
||
| Gaithersburg, MD : , : U.S. Dept. of Commerce, National Institute of Standards and Technology, , 1957 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Self-ignition properties of two propellant types / / A.F. Robertson, J. Loftus
| Self-ignition properties of two propellant types / / A.F. Robertson, J. Loftus |
| Autore | Robertson A. F |
| Pubbl/distr/stampa | Gaithersburg, MD : , : U.S. Dept. of Commerce, National Institute of Standards and Technology, , 1958 |
| Descrizione fisica | 1 online resource |
| Altri autori (Persone) |
LoftusJ
RobertsonA. F |
| Collana | NBS report |
| Soggetto topico | Solid propellants - Combustion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910711146503321 |
|
Robertson A. F
|
||
| Gaithersburg, MD : , : U.S. Dept. of Commerce, National Institute of Standards and Technology, , 1958 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||