Rocket exhaust plume phenomenology

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Bibliographic Details
Main Author: Simmons, Frederick S.
Format: eBook
Language: English
Published: El Segundo, Calif. : Reston, Va. : Aerospace Press ; American Institute of Aeronautics and Astronautics, ©2000.
Subjects:
Gas dynamics.
Plumes (Fluid dynamics)
Rocket engines > Exhaust emissions.
Rockets (Aeronautics)
elektronické knihy
electronic books
ISBN: 9781615832613
Physical Description: 1 online zdroj (xi, 286 pages) : illustrations

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Table of contents

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020 |a 9781615832613  |q (ebook) 
035 |a (OCoLC)555545457  |z (OCoLC)606252777  |z (OCoLC)649951633 
040 |a AU@  |b eng  |e pn  |c AU@  |d KNOVL  |d COO  |d OCLCQ  |d VLB  |d OCLCQ  |d KNOVL  |d OCLCE  |d OCLCO  |d KNOVL  |d OCLCF  |d OCLCQ 
100 1 |a Simmons, Frederick S. 
245 1 0 |a Rocket exhaust plume phenomenology  |h [elektronický zdroj] /  |c Frederick S. Simmons. 
260 |a El Segundo, Calif. :  |b Aerospace Press ;  |a Reston, Va. :  |b American Institute of Aeronautics and Astronautics,  |c ©2000. 
300 |a 1 online zdroj (xi, 286 pages) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
504 |a Includes bibliographical references and index. 
505 0 0 |t Rocket engines --  |t Characteristics of exhaust fumes --  |t Radiation processes --  |t Nozzle flow codes --  |t Plume models --  |t Signature scaling --  |t Time-varying properties of plumes --  |t Properties of molecular plume constituents --  |t Carbon soot properties --  |t Properties of alumina particles --  |t Diagnostic techniques for exit-plane exhaust --  |t Ultraviolet properties of plumes --  |t Post-boost phenomena --  |t Databases. 
520 8 |a Annotation  |b Presents an introductory treatment of plume phenomenology as it relates to the development of space-based defense systems. Covers elementary principles of rocketry, basics of rocket-propellant combustion, gas dynamics of supersonic exhaust plumes, infrared radiation processes, and diagnostic measurement techniques. Material is written at a level intended to bridge the gap between the needs of space systems engineers and the knowledge of scientists involved in detailed studies of plume observables. Simmons is a consultant in the private sector, and has been a consultant to Air Force space-based defense programs. Annotation c. Book News, Inc., Portland, OR (booknews.com). 
520 8 |a Annotation  |b This new book deals with the phenomenology of rocket exhaust plumes as the targets of space-based surveillance systems. Topics include the physical and chemical processes in rocket engines and their exhaust plumes, particularly in regard to flow properties, gas dynamics, and radiative mechanisms that are responsible for the generation of emission in rocket exhaust plumes at infrared and other wavelengths. System designers in a number of defense-related areas will be able to put the information in this book to immediate use. 
533 |a Electronic reproduction.  |b [S.l.] :  |c HathiTrust Digital Library,  |d 2010.  |5 MiAaHDL 
538 |a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.  |u https://proxy.k.utb.cz/login?url=http://purl.oclc.org/DLF/benchrepro0212  |5 MiAaHDL 
583 1 |a digitized  |c 2010  |h HathiTrust Digital Library  |l committed to preserve  |2 pda  |5 MiAaHDL 
588 |a Description based on print version record. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty univerzity 
650 0 |a Gas dynamics. 
650 0 |a Plumes (Fluid dynamics) 
650 0 |a Rocket engines  |x Exhaust emissions. 
650 0 |a Rockets (Aeronautics) 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
776 0 8 |i Print version:  |a Simmons, Frederick S.  |t Rocket exhaust plume phenomenology.  |d El Segundo, Calif. : Aerospace Press, ©2000  |z 188498908X  |w (DLC) 98074945  |w (OCoLC)44441055 
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999 |c 73800  |d 73800 
993 |x NEPOSILAT  |y EIZ 

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