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KSIĄŻKA JEST DOSTĘPNA NA ZEWNĘTRZNEJ PLATFORMIE. KSIĄŻKA NIE JEST W POSTACI PLIKU.

Solid Propellant Rocket Research

• Autorzy: Summerfield, Martin
• Wydawnictwo: Elsevier S & T
• Data wydania:
• Wydanie:
• Liczba stron: 712
• Forma publikacji: PDF (online)
• Język publikacji: angielski
• ISBN: 9780323163354

• Solid Propellant Rocket Research
• Copyright Page
• Table of Contents
• AMERICAN ROCKET SOCIETY: Solid Rockets Committee
• Solid Rockets Committee and Symposium Papers Committee
• CONTRIBUTORS TO VOLUME 1
• PREFACE TO THE SERIES
• PREFACE TO THE VOLUME
• PART A: MECHANICAL PROPERTIES OF GRAINS
• CHAPTER 1. GRAIN DESIGN AND DEVELOPMENT PROBLEMS FOR VERY LARGE ROCKET MOTORS
• ABSTRACT
• INTRODUCTION
• MOTOR HARDWARE
• MONOLITHIC GRAINS
• COMPARTMENTED GRAIN
• MODULAR GRAIN
• CONCLUSIONS
• REFERENCES
• CHAPTER 2. ON "POISSON!S RATIO" IN LINEAR VISCO-ELASTIC PROPELLANTS
• Abstract
• 1. "Poisson's Ratio" in Linear Visco-Elasticity
• 2. Evaluation of "Poisson's ratio" for Simple Elastically Compressible Visco-Elastic Media
• 3. Lateral Pressure on Thin-Walled Container due to Uni-Axial Compression of Simple Linear Visco-Ela
• 4. Linear Visco-Elastic Propellants with Continuous Distribution of Relaxation Times
• 5. Concluding Remarks
• References
• CHAPTER 3. MECHANICAL PROPERTIES AND THE DESIGN OF SOLID PROPELLANT MOTORS
• Abstract
• Introduction
• Background
• Strain Analysis
• Model Representation
• Ignition Analysis
• Slump and Inertia
• Thermal Strains
• Failure Analysis
• One to Three Dimensional Failure Association
• Conclusion
• REFERENCES
• CHAPTER 4. A METHOD OF STRENGTH ANALYSIS OF SOLID PROPELLANT ROCKET GRAINS
• ABSTRACT
• Introduction
• Criteria of Failure
• Effects of Internal Pressure
• Effects of Temperature Cycling
• Effects of Geometrical Irregularities
• Determination of Limiting Pressure
• Concluding Remarks
• Nomenclature
• Bibliography
• Reference Textbooks
• CHAPTER 5. STRESS AND STRAIN ANALYSIS OF CYLINDRICAL CASE-BONDED GRAINS
• A/ Ideally rigid chamber
• B/ Influence of k
• C/ Influence of m and m'
• D/ Influence of E/E'
• E/ Influence of the liner
• F/ Conclusions
• ANNEX I. INFLUENCE OF THE LINER
• ANNEX II. DETERMINATION OF k
• References
• PART B: STEADY-STATE BURNING MECHANISMS
• CHAPTER 6. BURNING MECHANISM OF AMMONIUM PERCHLORATE PROPELLANTS'
• ABSTRACT
• I. Structure of the Burning Zone of an Ammonium Perchlorate PropelIant
• Introduction
• Conditions at the Burning Surface
• Temperature Profile of the Reaction Zone (Thermocouple Method)
• Temperature Profile of the Reaction Zone (Thermocouple Method)
• Temperature Profile of Gaseous Reaction Layer ( Optical Method)
• Spectrographic Scanning of the Flame Zone
• II. Theory of Burning of a Composite Solid Propellant
• Physico-chemical Model of the Flame
• AnaIysis
• Possible Tests of the Theory
• Other Attempts at a Theory of Burning
• ExperimentaI Method
• Effects of Particle Size and Fuel-Qxidant Ratio
• Effect of Particle Size Distribution
• Effect of Copper Chromite Catalyst
• ConcIusions
• Note Added in Proof
• References
• CHAPTER 7. SOME RESEARCH PROBLEMS IN THE STEADY-STATE BURNING OF COMPOSITE SOLID PROPELLANTS
• ABSTRACT
• A. Introduction
• B. Study of Techniques of Measurements with a Strand Burner
• C. Measurement of Burning Rates in a Radial Burning Grain
• D. The Study of Particle Size Effects on Burning Rates
• E. The Effect of Radiation Upon the Burning Rate of Composite Solid Propellants
• F. Conclusion
• Note Added in Proof
• REFERENCES
• CHAPTER 8. A THEORETICAL STUDY OF THE BURNING OF A SOLID PROPELLANT SANDWICH
• ABSTRACT
• NOMENCLATURE
• 1. INTRODUCTION
• 2. STATEMENT OF SANDWICH PROPELLANT PROBLEM
• 3. COMBINED CONCENTRATION AND TEMPERATURE FIELDS
• 4. BURNING RATE – SURFACE TEMPERATURE RELATION
• 5. DEPRESSION OF FUEL SLAB SURFACES
• 6. CONCLUSION
• REFERENCES
• CHAPTER 9. THE ROLE OF BINDER IN COMPOSITE PROPELLANT COMBUSTION
• ABSTRACT
• INTRODUCTION
• "TWO-TEMPERATURE POSTULATE AND "THERMAL LAYER" THEORY OF COMBUSTION
• THE INFLUENCE OF BINDER ON THE THERMAL LAYER
• APPLICATION TO EXPERIMENTAL BURNING RATE DATA
• PHYSICAL ROLE OF BINDER IN PROPELLANT BURNING
• ACKNOWLEDGEMENT
• REFERENCES
• PART C: COMBUSTION OF METALS
• CHAPTER 10. COMBUSTION OF METALS: PHYSICAL CONSIDERATIONS
• 1 . Associate Professor, Department of Aeronautical Engineering , Member ARS.
• 2. The author would like to thank the Research Laboratories of the United Aircraft Corp. for perform
• REFERENCES
• CHAPTER 11. THE EXPERIMENTAL NATURE OF THE COMBUSTION OF METALLIC POWDERS
• INTRODUCTION
• EXPERIMENTAL
• METALLOGRAPHIC STUDY OF COMBUSTION PRODUCTS
• X-RAY DIFFRACTION STUDIES OF THE COMBUSTION PRODUCTS
• THERMODYNAMIC CALCULATIONS OF ADIABATIC COMBUSTION TEMPERATURES
• SUMMARY AND CONCLUSIONS
• PROPOSED MODEL
• CHAPTER 12. COMBUSTION CHARACTERISTICS OF METAL PARTICLES
• I. Chemist, Poulter Laboratory, Propulsion Division
• CHAPTER 13. THE COMBUSTION OF ELEMENTAL BORON
• I. Senior Scientist
• Rate-Limiting Steps
• Region I
• Region II
• Region III
• Region IV
• Region V
• Ignition Temperature
• REFERENCES
• CHAPTER 14. METAL COMBUSTION IN DEFLAGRATING PROPELLANT
• I. Chemist, Combustion Group
• PART D: THEORIES OF UNSTABLE COMBUSTION
• CHAPTER 15. SOUD PROPELLANT ROCKET MOTORS AS ACOUSTIC OSCILLATORS
• ABSTRACT
• SOLED PROPELLANT ROCKET MOTORS AS ACOUSTIC OSCILLATORS
• I. INTRODUCTION
• II. APERÇU
• III. ACOUSTIC RESPONSE OF THE BURNING SURFACE
• IV. ACOUSTIC MODES OF SOLID PROPELLANT ROCKETS
• V. ACOUSTIC STABILITY OF THE GAS QUASI-MODES
• VI. EFFECTS AT HIGH AMPLITUDE
• VII. CONCLUDING REMARKS
• ACKNOWLEDGMENT
• References
• CHAPTER 16. HEAT TRANSFER STABILITY ANALYSIS OF SOLID PROPELLANT ROCKET MOTORS
• Introduction
• The Equations for Heat Transfer at the Surface of a Burning Propellant
• Steady State Solutions
• Stability Analysis of Small Perturbations
• ConcIusions
• Acknowledgment
• Nomenclature
• Bibliography
• CHAPTER 17. A THEORY OF OSCILLATORY BURNING OF SOLID PROPELLANTS ASSUMING A CONSTANT SURFACE TEMPERA
• SUMMARY
• Introduction
• Discussion
• References
• CHAPTER 18. COMBUSTION INSTABILITY IN SOLID ROCKETS USING PROPELLANTS WITH REACTIVE ADDITIVES
• SUMMARY
• SYMBOL LIST
• I. INTRODUCTION
• II. PHYSICAL VISUALIZATION AND GENERAL SCHEME OF ANALYSIS
• III. MODEL WITH INSENSITIVE HEAT SOURCES
• IV. MODEL WITH SENSITIVE HEAT SOURCES
• V. CONCLUDING REMARKS
• APPENDIX: Analysis With Distributed, Sensitive Heat Source Model
• References
• CHAPTER 19. THE INFLUENCE OF EROSIVE BURNING ON ACOUSTIC INSTABILITY IN SOLID PROPELLANT ROCKET MOTO
• ABSTRACT
• I. INTRODUCTION
• II. ANALYTICAL FORMULATION
• III. ANALYTICAL SOLUTION OF THE BOUNDARY VALUE PROBLEM
• IV. RESULTS OBTAINED FROM THE ANALYTICAL SOLUTION OF BOUNDARY VALUE PROBLEM (NON-DEGENERATE CASE)
• V. THE DEGENERATE CASE
• VI. DISCUSSION
• ACKNOWLEDGMENT
• REFERENCES
• PART E: EXPERIMENTS ON UNSTABLE BURNING
• CHAPTER 20. AN EXPERIMENTAL INVESTIGATION OF UNSTABLE COMBUSTION IN SOLID PROPELLANT ROCKET MOTORS
• ABSTRACT
• INTRODUCTION
• CHARACTERISTIC FEATURES OF THE UNSTABLE FIRINGS
• REPRODUCIBILITY OF THE EXPERIMENTS
• RESULTS OF INSTABILITY EXPERIMENTS
• MOTORS WITH OPPOSED-PLANE GRAIN DESIGNS
• CONCLUSIONS AND CONCLUDING REMARKS
• NOMENCLATURE
• REFERENCES
• CHAPTER 21. EXPERIMENTAL INVESTIGATIONS OF UNSTABLE BURNING IN SOLID PROPELLANT ROCKET MOTORS
• ABSTRACT
• I. INTRODUCTION
• II. EXPERIMENTAL RESULTS
• III. THEORETICAL STUDIES
• IV. SUMMARY
• ACKNOWLEDGEMENT
• NOMENCLATURE
• REFERENCES
• CHAPTER 22. UNSTABLE BURNING PHENOMENON IN DOUBLE-BASE PROPELLANTS
• ABSTRACT
• I INTRODUCTION
• II BACKGROUND ON UNSTABLE BURNING
• III THE EXPERIMENTAL ROCKET
• IV SUPPRESSION OF UNSTABLE BURNING
• V CONCLUSION AND RECOMMENDATIONS
• Acknowledgment
• References
• CHAPTER 23. REVIEW OF EXPERIMENTAL RESEARCH ON COMBUSTION INSTABILITY OF SOLID PROPELLANTS
• INTRODUCTION
• STATUS OF THE THEORY
• PRACTICAL RESULTS OF EXPERIMENTAL RESEARCH
• THE COMBUSTION ZONE DURING STEADY STATE COMBUSTION
• UNSTEADY COMBUSTION
• ACOUSTICS
• DAMPING PROCESSES
• CONCLUSION
• ACKNOWLEDGMENT
• REFERENCES
• CHAPTER 24. RESONANT BURNING OF SOLID PROPELLANTS: REVIEW OF CAUSES, CURES AND EFFECTS
• ABSTRACT
• DEFINITIONS AND TERMINOLOGY
• SPECULATIONS CONCERNING A PHYSICAL DESCRIPTION
• OCCURRENCE OF THE OSCILLATORY PHENOMENON
• OCCURRENCE OF THE IRREGULAR PHENOMENON
• FACTORS THAT AFFECT OCCURRENCE OF UNSTABLE OPERATION
• REPRODUCIBILITY
• CONCLUDING REMARKS
• REFERENCES
• PART F: SOLID PROPELLANT IGNITION
• CHAPTER 25. THE MECHANISM OF IGNITION OF COMPOSITE SOLID PROPELLANTS
• ABSTRACT
• I. INTRODUCTION
• II. EXPERIMENTAL METHOD
• III. THE GAS PHASE THEORY OF IGNITION
• IV. EXPERIMENTAL RESULTS AND COMPARISON WITH THEORY
• V. IMPLICATIONS OF THE GAS PHASE IGNITION THEORY
• VI. CONCLUSIONS
• REFERENCES
• CHAPTER 26. PROPELLANT IGNITION BY HIGH CONVECTIVE HEAT FLUXES
• Abstract
• Propellant Ignition by High Convective Heat Fluxes
• Summary
• Nomenclature
• References
• CHAPTER 27. SOLID PROPELLANT IGNITION STUDIES WITH HIGH FLUX RADIANT ENERGY AS A THERMAL SOURCE
• Abstract
• Background
• Equipment
• Ignition Studies Using the Arc-Image Furnace
• Temperature
• Gas Composition
• Delay Time
• Other Experimental Techniques
• Acknowledgement
• REFERENCES

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