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Fundamentals of hybrid rocket combustion and Propulsion.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Chiaverini, Martin J.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Reston : American Institute of Aeronautics and Astronautics, 2000.
Temas:
Acceso en línea:Texto completo

MARC

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100 1 |a Chiaverini, Martin J. 
245 1 0 |a Fundamentals of hybrid rocket combustion and Propulsion. 
260 |a Reston :  |b American Institute of Aeronautics and Astronautics,  |c 2000. 
300 |a 1 online resource (665 pages) 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
588 0 |a Print version record. 
505 0 |a ""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"" 
505 8 |a ""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"" 
505 8 |a ""Chapter 14. Flight Testing of Hybrid-Powered Vehicles""""Chapter 15. Challenges of Hybrid Rocket Propulsion in the 21st Century""; ""Index"" 
590 |a ProQuest Ebook Central  |b Ebook Central Academic Complete 
650 0 |a Hybrid propellant rockets. 
650 0 |a Rocket engines  |x Combustion. 
650 0 |a Rockets (Aeronautics)  |x Fuel. 
650 6 |a Fusées à propergol hybride. 
650 6 |a Moteurs-fusées  |x Combustion. 
650 6 |a Fusées (Aéronautique)  |x Combustibles. 
650 7 |a Hybrid propellant rockets  |2 fast 
650 7 |a Rocket engines  |x Combustion  |2 fast 
650 7 |a Rockets (Aeronautics)  |x Fuel  |2 fast 
758 |i has work:  |a Fundamentals of hybrid rocket combustion and propulsion (Text)  |1 https://id.oclc.org/worldcat/entity/E39PCFQHFkrPqcXkBDwJbt8YKd  |4 https://id.oclc.org/worldcat/ontology/hasWork 
776 0 8 |i Print version:  |a Chiaverini, Martin J.  |t Fundamentals of hybrid rocket combustion and Propulsion.  |d Reston : American Institute of Aeronautics and Astronautics, ©2000  |z 9781563477034 
856 4 0 |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111541  |z Texto completo 
938 |a ProQuest Ebook Central  |b EBLB  |n EBL3111541 
994 |a 92  |b IZTAP