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



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Titolo: Fundamentals of hybrid rocket combustion and propulsion [[electronic resource] /] / edited by Martin J. Chiaverini, Kenneth K. Kuo Visualizza cluster
Pubblicazione: Reston, Va., : American Institute of Aeronautics and Astronautics, c2007
Descrizione fisica: 1 online resource (665 p.)
Disciplina: 629.47/52
Soggetto topico: Hybrid propellant rockets
Rocket engines - Combustion
Rockets (Aeronautics) - Fuel
Soggetto genere / forma: Electronic books.
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""
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.: 9910456604703321
Lo trovi qui: Univ. Federico II
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Serie: Progress in astronautics and aeronautics ; ; v. 218.