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Analytical and numerical assessment of axial thrust balancing systems in liquid rocket engine LOx turbopumps

Maier, Sebastian and Wagner, Bernd and Veggi, Lucrezia and Pauw, Julian (2017) Analytical and numerical assessment of axial thrust balancing systems in liquid rocket engine LOx turbopumps. 7th European Conference for Aeronautics and Space Sciences (EUCASS), 03.-06. Jul. 2017, Mailand, Italien.

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Item URL in elib:https://elib.dlr.de/117169/
Document Type:Conference or Workshop Item (Speech)
Title:Analytical and numerical assessment of axial thrust balancing systems in liquid rocket engine LOx turbopumps
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Maier, SebastianInstitut für Raumfahrtantriebe, DLR Lampoldshausen, DUNSPECIFIED
Wagner, BerndBernd.Wagner (at) dlr.dehttps://orcid.org/0000-0003-3431-5898
Veggi, LucreziaUNSPECIFIEDUNSPECIFIED
Pauw, JulianUNSPECIFIEDUNSPECIFIED
Date:3 July 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, balancing System, CFD, validation
Event Title:7th European Conference for Aeronautics and Space Sciences (EUCASS)
Event Location:Mailand, Italien
Event Type:international Conference
Event Dates:03.-06. Jul. 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 > Leitungsbereich RA
Deposited By: Hanke, Michaela
Deposited On:13 Dec 2017 08:07
Last Modified:13 Dec 2017 08:07

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