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Assessment of performance variation on the axial and radial forces in turbopump configurations for liquid rocket engines

Wagner, Bernd and Veggi, Lucrezia and Pauw, Julian (2017) Assessment of performance variation on the axial and radial forces in turbopump configurations for liquid rocket engines. 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC), 16. - 21. Dez. 2017, Maui, USA.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/117152/
Document Type:Conference or Workshop Item (Speech)
Title:Assessment of performance variation on the axial and radial forces in turbopump configurations for liquid rocket engines
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wagner, BerndBernd.Wagner (at) dlr.dehttps://orcid.org/0000-0003-3431-5898
Veggi, LucreziaUNSPECIFIEDUNSPECIFIED
Pauw, JulianUNSPECIFIEDUNSPECIFIED
Date:2017
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:turbopump, axial thrust, radial thrust
Event Title:17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC)
Event Location:Maui, USA
Event Type:international Conference
Event Dates:16. - 21. Dez. 2017
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:13 Dec 2017 08:06
Last Modified:13 Dec 2017 08:06

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