Please use this identifier to cite or link to this item: http://hdl.handle.net/2440/43531
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Type: Journal article
Title: Steady-state high pressure LOx/H2 rocket engine combustion
Author: Smith, Joshua John
Schneider, Gerald Manfred
Suslov, D.
Oschwald, M.
Haidn, O.
Citation: Aerospace Science and Technology, 2007; 11 (1):39-47
Part of: Propellant combustion phenomena / Luigi T. DeLuca, Paul Kuentzmann and Alexander S. Rudakov (eds.)
Publisher: Editions Scientifiques Medicales Elsevier
Issue Date: 2007
ISSN: 1270-9638
School/Discipline: School of Mechanical Engineering
Statement of
Responsibility: 
Joshua J. Smith, Gerald Schneider, Dmitry Suslov, Michael Oschwald and Oskar Haidn
Description: Copyright © 2006 Elsevier Masson SAS All rights reserved.
RMID: 0020070439
DOI: 10.1016/j.ast.2006.08.007
Description (link): http://www.elsevier.com/wps/find/journaldescription.cws_home/600735/description#description
Appears in Collections:Mechanical Engineering publications

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