000			03027nam a2200481 a 4500
001			EBC3111571
003			MiAaPQ
005			20240121042411.0
006			m o d |
007			cr cn|||||||||
008			101023s2007 vaua sb 001 0 eng d
010			_z 2010501922
020			_z1563479214
020			_z9781563479212
020			_a9781600864711 (electronic bk.)
035			_a(MiAaPQ)EBC3111571
035			_a(Au-PeEL)EBL3111571
035			_a(CaPaEBR)ebr10516675
035			_a(OCoLC)922978803
040			_aMiAaPQ _cMiAaPQ _dMiAaPQ
043			_ae-ur---
050		4	_aTL783.4 _b.D73 2007
082	0	4	_a621.43/56 _223
100	1		_aDranovsky, Mark L.
245	1	0	_aCombustion instabilities in liquid rocket engines _h[electronic resource] : _btesting and development practices in Russia / _cMark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley.
260			_aReston, Va. : _bAmerican Institute of Aeronautics and Astronautics, _cc2007.
300			_axix, 321 p. : _bill.
490	1		_aProgress in astronautics and aeronautics ; _vv. 221
504			_aIncludes bibliographical references and index.
505	0		_aIntroduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine.
533			_aElectronic reproduction. Ann Arbor, MI : ProQuest, 2015. Available via World Wide Web. Access may be limited to ProQuest affiliated libraries.
650		0	_aLiquid propellant rockets.
650		0	_aRocket engines _xCombustion _zRussia (Federation) _xTesting.
650		0	_aLiquid fuels _xCombustion _zRussia (Federation) _xTesting.
650		0	_aRockets (Aeronautics) _zRussia (Federation) _xTesting.
655		4	_aElectronic books.
700	1		_aYang, Vigor.
700	1		_aCulick, F. _q(Fred), _d1933-
700	1		_aTalley, Douglas G.
710	2		_aProQuest (Firm)
830		0	_aProgress in astronautics and aeronautics.
856	4	0	_uhttps://ebookcentral.proquest.com/lib/bacm-ebooks/detail.action?docID=3111571 _zClick to View
999			_c169157 _d169158