000			03635nam a22005173i 4500
001			EBC3111571
003			MiAaPQ
005			20240729124522.0
006			m o d |
007			cr cnu||||||||
008			240724s2000 xx o ||||0 eng d
020			_a9781600864711 _q(electronic bk.)
020			_z9781563479212
035			_a(MiAaPQ)EBC3111571
035			_a(Au-PeEL)EBL3111571
035			_a(CaPaEBR)ebr10516675
035			_a(OCoLC)922978803
040			_aMiAaPQ _beng _erda _epn _cMiAaPQ _dMiAaPQ
050		4	_aTL783.4 -- .D73 2007eb
082	0		_a621.43/56
100	1		_aDranovsky, Mark L.
245	1	0	_aCombustion Instabilities in Liquid Rocket Engines : _bTesting and Development Practices in Russia.
250			_a1st ed.
264		1	_aReston : _bAmerican Institute of Aeronautics and Astronautics, _c2000.
264		4	_c©2007.
300			_a1 online resource (342 pages)
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
490	1		_aProgress in Astronautics and Aeronautics
505	0		_aCover -- Title -- Copyright -- Foreword -- Table of Contents -- Preface -- Acknowledgments -- Acronyms and Abbreviations -- Chapter 1. Introduction -- Chapter 2. Terms and Definitions -- Chapter 3. Mechanisms of Transition from Noise to High-Frequency Oscillations or to Noise at a New Level -- Chapter 4. Uncertainty in Conversion of Propellant to Combustion Products -- Chapter 5. Studies of Operating Process Stability at Various Stages of Combustor Development -- Chapter 6. Quantitative Characteristics for Estimating Stability of LRE Combustion Chambers and Gas Generators -- Chapter 7. Acoustic Study of Combustion Chamber Stability Characteristics -- Chapter 8. Determination of Stability of Oscillations from Natural Disturbances -- Chapter 9. Evaluation of LRE Process Stability by Use of Artificial Pressure Disturbances -- Chapter 10. Model Firing Tests for Selection of Injector Head Elements -- Chapter 11. Estimation of Operating Process Stability from Pressure Oscillation Decrements -- Chapter 12. Test Results for Pulsing Liquid-Liquid Chambers -- Chapter 13. Stability of Gas-Liquid Combustion Chambers -- Chapter 14 Gas-Liquid Combustion-Chamber Tests for Stability to Hard Excitation -- Chapter 15. Injector Head for RD-170 Engine Combustion Chamber -- Chapter 16. Stability Characteristics of Engines with Adjustable Injectors -- Chapter 17. Control of Stability in Production of the Proton Engine -- References -- Bibliography -- Index -- Supporting Materials.
588			_aDescription based on publisher supplied metadata and other sources.
590			_aElectronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
650		0	_aLiquid propellant rockets.
650		0	_aRocket engines -- Combustion -- Russia (Federation) -- Testing.
650		0	_aLiquid fuels -- Combustion -- Russia (Federation) -- Testing.
650		0	_aRockets (Aeronautics) -- Russia (Federation) -- Testing.
655		4	_aElectronic books.
700	1		_aYang, Vigor.
700	1		_aCulick, F.
700	1		_aTalley, Douglas G.
776	0	8	_iPrint version: _aDranovsky, Mark L. _tCombustion Instabilities in Liquid Rocket Engines _dReston : American Institute of Aeronautics and Astronautics,c2000 _z9781563479212
797	2		_aProQuest (Firm)
830		0	_aProgress in Astronautics and Aeronautics
856	4	0	_uhttps://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111571 _zClick to View
999			_c68238 _d68238