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Combustion efficiency of a porous injector during throttling of a LOX/H2 combustion chamber

Deeken, J. and Haidn, O. and Schlechtriem, S. and Suslov, D. (2011) Combustion efficiency of a porous injector during throttling of a LOX/H2 combustion chamber. In: EUCASS EUCASS Advances in Aerospace Sciences, Vol. 2 - Propulsion Physics. pp. 251-264.

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Document Type:Book Section
Title:Combustion efficiency of a porous injector during throttling of a LOX/H2 combustion chamber
Authors:
AuthorsInstitution or Email of Authors
Deeken, J.Jan.Deeken@dlr.de
Haidn, O.Oskar.Haidn@dlr.de
Schlechtriem, S.Stefan.Schlechtriem@dlr.de
Suslov, D.Dmitry.Suslov@dlr.de
Date:2011
Journal or Publication Title:EUCASS
Refereed publication:Yes
In ISI Web of Science:No
Volume:Vol. 2 - Propulsion Physics
Page Range:pp. 251-264
Series Name:EUCASS Advances in Aerospace Sciences
Status:Published
Keywords:combustion, porous injector, H2/O2
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Michaela Hanke
Deposited On:16 Dec 2010 12:45
Last Modified:13 Dec 2011 08:31

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