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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), 2017-12-16 - 2017-12-21, Maui, USA.

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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 AuthorsAuthor's ORCID iDORCID Put Code
Wagner, BerndUNSPECIFIEDhttps://orcid.org/0000-0003-3431-5898UNSPECIFIED
Veggi, LucreziaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Pauw, JulianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
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 Start Date:16 December 2017
Event End Date:21 December 2017
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:13 Dec 2017 08:06
Last Modified:24 Apr 2024 20:21

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