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The chemistry of propellants : a meeting organised by the AGARD Combustion and Propulsion Panel, Paris, France, June 8-12, 1959 /
The Chemistry of Propellants is a collection of papers and comments presented at the meeting on "The Chemistry of Propellants”, held in Paris, France on June 8-12, 1959, organized by the AGARD Combustion and Propulsion Panel. This book is organized into six parts encompassing 25 chapte...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor Corporativo: | |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Oxford ; New York :
Pergamon Press,
1960.
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| Colección: | Combustion and propulsion researches and reviews ;
1959. |
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Front Cover; The Chemistry of Propellants; Copyright Page; Table of Contets; PART 3: SOLID PROPELLANTS; PART 4: PROPELLANTS FOR AIR-BREATHING ENGINES; PART 5: SELECTED BASIC STUDIES; PART 6: HIGH-ENERGY PROPELLANTS AND BASIC PROPULSION PROBLEMS; PREFACE; EDITORS' NOTE; INTRODUCTION; OPENING REMARKS MADE BY DR. FREDERICK SEITZ, NATOSCIENCE ADVISOR, AT THE AGARD MEETING ON CHEMISTRY OF PROPELLANTS
- PART 1: PROPELLANT SOURCES AND COSTS; CHAPTER 1. SOURCES, AVAILABILITY AND ESTIMATED COSTS OF PROPELLANTS; INTRODUCTION; PROPELLANT COST. RATE OF PRODUCTION RELATIONSHIP.
- Cost of improving performancesystem cost implications; current annual united stases' production; availability and cost of specific fuels and oxidamts; summary; references; part 2: liquid propellants; chapter 2. high temperature thermodynamics and theoretical performance evaluation of rocket propellants; abstract; sommaire; nomenclature; high temperature thermodynamics and theoretical performance evaluation of rocket propellants; introduction; theoretical performance calculations; model assumptions; method of calculation; calculation of chamber conditions; calculation of nozzle conditions.
- CALCULATION OF PERFORMANCE PARAMETERSRESULTS OF THERMODYNAMIC CALCULATIONS; CHAPTER 3. THERMODYNAMIC PROPERTIES OF COMBUSTION PRODUCTS; ALUMINUM; RESULTS AND USE OF PERFORMANCE DATA; FUTURE EXTENSIONS OF GENERALIZED N-ELEMENT PROGRAM; ACKNOWLEDGEMENT; REFERENCES; CHAPT3ER 4. PAGE 1 OF APPENDIX B TABLE I
- CHAMBER CONDITIONS; APPENDIX C: Cathode Ray Tube Traces; CHAPTER 5. LIQUID PROPELL ANTS FOR ROCKETS; i . INTRODUCTION; 2. PERTINENT PROPERTIES OF LIQUID PROPELLANTS; 3� PREPARATION OF LIQUID PROPELLANTS; 4. PERFORMANCE; 5. RECOMMENDATIONS; 6� CONCLUSION; SOMMAIRE; REFERENCES.
- Chapter 6. an experimental evaluation of rocket propellant dataabstract; sommaire; introductory remarks; program background; scope of the fuels evaluation program; selection of test fuels; combustion stability evaluation; heat transfer and coolant property tests; research thrust chamber performance evaluation; gas generator performance and thermodynamic gas properties; concluding remarks; acknowledgment; bibliography; appendix a: laboratory analysis of test fuels; chapter 7. discussion of the paper; discussions of the paper by d. l. armstrong; moureu and r.levy: comments on greenfield'spaper.
- DISCUSSIONS OF THE PAPER BY S. GREENFIELDCHAPTER 8. PREPARATION AND PROPERTIES OF DOUBLE-BASE PROPELLANTS; INTRODUCTION; PREPARATION; PHYSICAL PROPERTIES; SURVEILLANCE PROPERTIES; CONCLUSION; References; CHAPTER 9. PREPARATION ET PROPRIETES DES PROPERGOLS: PROPERGOIS SOLIDES COMPOSITES; 1. GENERALITES; 2. FABRICATION DES PROPKHGOLS SOLIDES COMPOSITES; 3. PROPRIETES DES POUDRES COMPOSITES; 4. BIBLIOGRAPHIE; SUMMARY; CHAPTER 10. METHODS OF BURNING RATE CONTROL IN SOLID PROPELLANTS; ABSTRACT; INTRODUCTION; CHAPTER 11. METHODS OF BURNING RATE CONTROL IN SOLID PROPELLANTS.