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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: 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 AuthorsAuthor's ORCID iDORCID Put Code
Gröning, StefanInstitut für Raumfahrtantriebe, DLR LampoldshausenUNSPECIFIEDUNSPECIFIED
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Suslov, DmitryUNSPECIFIEDhttps://orcid.org/0000-0002-5160-9292UNSPECIFIED
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825UNSPECIFIED
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:Yes
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 Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:16 Nov 2016 07:49
Last Modified:21 Nov 2023 10:29

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