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Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen

Gröning, Stefan and Hardi, Justin and Suslov, Dmitry and Oschwald, Michael (2016) Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen. CEAS Space Journal. Springer. DOI: DOI 10.1007/s12567-016-0130-8 ISSN 1868-2502

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Item URL in elib:https://elib.dlr.de/107791/
Document Type:Article
Title:Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gröning, StefanInstitut für Raumfahrtantriebe, DLR LampoldshausenUNSPECIFIED
Hardi, JustinJustin.Hardi (at) dlr.deUNSPECIFIED
Suslov, DmitryDmitry.Suslov (at) dlr.deUNSPECIFIED
Oschwald, MichaelMichael.Oschwald (at) dlr.deUNSPECIFIED
Date:2016
Journal or Publication Title:CEAS Space Journal
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI :DOI 10.1007/s12567-016-0130-8
Publisher:Springer
ISSN:1868-2502
Status:Published
Keywords:Combustion instabilities · Hydrogen temperature ramping · Liquid propellant rocket engines
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:16 Nov 2016 07:49
Last Modified:16 Nov 2016 07:49

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