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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 (2017) Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen. CEAS Space Journal, pp. 59-76. Springer. DOI: 10.1007/s12567-016-0130-8 ISSN 1868-2502

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Item URL in elib:https://elib.dlr.de/114073/
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, StefanDLR, Institute of Space Propulsion, Lampoldshausen, GermanyUNSPECIFIED
Hardi, JustinDLR, Institute of Space Propulsion, Lampoldshausen, Germanyhttps://orcid.org/0000-0003-3258-5261
Suslov, DmitryDLR, Institute of Space Propulsion, Lampoldshausen, GermanyUNSPECIFIED
Oschwald, MichaelDLR, Institute of Space Propulsion, Lampoldshausen, Germanyhttps://orcid.org/0000-0002-9579-9825
Date:July 2017
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
Page Range:pp. 59-76
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 - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:18 Sep 2017 08:33
Last Modified:14 Dec 2019 04:28

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