000			01657nam a2200385 a 4500
001			EBC3111646
003			MiAaPQ
005			20240123100207.0
006			m o d |
007			cr cn|||||||||
008			120113s1995 dcuad sb 001 0 eng d
020			_z1563471833
020			_z9781563471834
020			_a9781600864186 (electronic bk.)
035			_a(MiAaPQ)EBC3111646
035			_a(Au-PeEL)EBL3111646
035			_a(CaPaEBR)ebr10516751
035			_a(OCoLC)922979061
040			_aMiAaPQ _cMiAaPQ _dMiAaPQ
050		4	_aTL783.4 _b.L57 1995
245	0	0	_aLiquid rocket engine combustion instability _h[electronic resource] / _cedited by Vigor Yang.
260			_aWashington, D.C. : _bAmerican Institute of Aeronautics and Astronautics, Inc., _c1995.
300			_a564 p. : _bill.
490	1		_aProgress in astronautics and aeronautics ; _vv. 169
504			_aIncludes bibliographical references and index.
505	0		_apt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology.
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.
655		4	_aElectronic books.
700	1		_aYoung, Vigor.
710	2		_aProQuest (Firm)
830		0	_aProgress in astronautics and aeronautics ; _vv. 169.
856	4	0	_uhttps://ebookcentral.proquest.com/lib/bacm-ebooks/detail.action?docID=3111646 _zClick to View
999			_c169308 _d169308