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Fundamentals of hybrid rocket combustion and propulsion / / edited by Martin J. Chiaverini, Kenneth K. Kuo



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Titolo: Fundamentals of hybrid rocket combustion and propulsion / / edited by Martin J. Chiaverini, Kenneth K. Kuo Visualizza cluster
Pubblicazione: Reston, Va., : American Institute of Aeronautics and Astronautics, c2007
Edizione: 1st ed.
Descrizione fisica: 1 online resource (665 p.)
Disciplina: 629.47/52
Soggetto topico: Hybrid propellant rockets
Rocket engines - Combustion
Rockets (Aeronautics) - Fuel
Altri autori: ChiaveriniMartin J <1968-> (Martin John)  
KuoKenneth K  
Note generali: Description based upon print version of record.
Nota di bibliografia: Includes bibliographical references and index.
Nota di contenuto: ""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Acknowledgements""; ""Table of Contents""; ""Chapter 1. Overview and History of Hybrid Rocket Propulsion""; ""Chapter 2. Review of Solid-Fuel Regression Rate Behavior in Classical and Nonclassical Hybrid Rocket Motors""; ""Chapter 3. Solid-Fuel Pyrolysis Phenomena and Regression Rate, Part 1: Mechanisms""; ""Chapter 4. Solid-Fuel Pyrolysis Phenomena and Regression Rate, Part 2: Measurement Techniques""; ""Chapter 5. Analytical Models for Hybrid Rockets""; ""Chapter 6. Vortex Injection Hybrid Rockets""
""Chapter 7. High-Speed Flow Effects in Hybrid Rockets""""Chapter 8. Computational Fluid Dynamics Modeling of Hybrid Rocket Flowfields""; ""Chapter 9. Combustion Instability and Transient Behavior in Hybrid Rocket Motors""; ""Chapter 10. Metals, Energetic Additives, and Special Binders Used in Solid Fuels for Hybrid Rockets""; ""Chapter 11. Hydrogen Peroxide, Hydroxyl Ammonium Nitrate, and Other Storable Oxidizers""; ""Chapter 12. Similarity and Scaling Effects in Hybrid Rocket Motors""; ""Chapter 13. Large-Scale Hybrid Motor Testing""
""Chapter 14. Flight Testing of Hybrid-Powered Vehicles""""Chapter 15. Challenges of Hybrid Rocket Propulsion in the 21st Century""; ""Index""
Sommario/riassunto: Fundamentals of Hybrid Rocket Combustion and Propulsion is the first text to offer a comprehensive treatment of hybrid rockets. In this book, editors have pooled together some of the most respected minds in the field, each providing their very special insight and expertise to the text. The content is therefore as up-to-date as it is broad. Each chapter offers an expert account of every aspect of hybrid rocket propulsion, including fundamental aspects of hybrid combustion, numerical and theoretical approaches, and various applications. All chapters are enhanced with more than 25 to 35 graphical elements - including tables, figures and photographs. Making for an easy and informative read, this book is a must-have resource for anyone currently working in or studying rocket propulsion.
Titolo autorizzato: Fundamentals of hybrid rocket combustion and propulsion  Visualizza cluster
ISBN: 1-60086-687-5
1-60086-468-6
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910953225603321
Lo trovi qui: Univ. Federico II
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Serie: Progress in astronautics and aeronautics ; ; v. 218.