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Numerical calculation of the rotordynamic coefficients of a LOX-Turbopump Seal for the LUMEN LOX/LNG demonstrator rocket engine

Müller, Max Axel and Traudt, Tobias and Schlechtriem, Stefan (2020) Numerical calculation of the rotordynamic coefficients of a LOX-Turbopump Seal for the LUMEN LOX/LNG demonstrator rocket engine. In: 18th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery. 18th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 23. - 26. Nov. 2020, Online.

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Item URL in elib:https://elib.dlr.de/139820/
Document Type:Conference or Workshop Item (Speech)
Title:Numerical calculation of the rotordynamic coefficients of a LOX-Turbopump Seal for the LUMEN LOX/LNG demonstrator rocket engine
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Müller, Max AxelDLR, Inst. für Raumfahrtantriebe, Lampoldshausen, DUNSPECIFIED
Traudt, TobiasTobias.Traudt (at) dlr.dehttps://orcid.org/0000-0002-0206-0483
Schlechtriem, Stefanstefan.schlechtriem (at) dlr.dehttps://orcid.org/0000-0002-3714-9664
Date:2020
Journal or Publication Title:18th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:rocket engine, turbopump, liquid methane, LOX, rotordynamic, seal
Event Title:18th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery
Event Location:Online
Event Type:international Conference
Event Dates:23. - 26. Nov. 2020
Organizer:Pacific Center of Thermal-Fluids Engineering and Waseda University
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 - Project LUMEN (Liquid Upper Stage Demonstrator Engine)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute of Space Propulsion > Leitungsbereich RA
Deposited By: Hanke, Michaela
Deposited On:18 Dec 2020 08:55
Last Modified:18 Dec 2020 08:55

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