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DLR Project TAUROS: TAU for Rocket Thrust Chamber Simulation

Schneider, Dirk and Hardi, Justin and Martin, Jan and Stark, Ralf and Suslov, Dmitry and Tonti, Federica and Van Schyndel, Jan and Zhukov, Victor / V. P. and Oschwald, Michael and Costa Ruiz, Eugeni and Fechter, Stefan and Horchler, Tim and Karl, Sebastian and Hannemann, Klaus and Adler, Marko and Jack, Sebastian and Eggers, Thino and Lechtenberg, Ansgar and Gerlinger, Peter (2019) DLR Project TAUROS: TAU for Rocket Thrust Chamber Simulation. In: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. 8th European Conference for Aeronautics and Space Sciences EUCASS, 1. - 4. Jul. 2019, Madrid, Spain. doi: 10.13009/EUCASS2019-515.

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The present work gives a brief overview of the DLR (German Aerospace Center) project TAUROS (TAU for Rocket Thrust Chamber Simulation). The DLR project TAUROS is a collaboration between three different DLR institutes, and is funded by the DLR Space Research Programmatic. The project focuses on the qualification and advancement of the DLR flow solver TAU for liquid rocket thrust chamber application. The main objective of TAUROS is to ensure an independent DLR competence in the numerical modeling of space propulsion systems and their components. The collaboration bundles the DLR competences in the field of development and application of numerical methods for liquid space propulsion systems, and in the field of development and operation of research rocket thrust chambers. This ensures a verification and validation of the developed numerical methods independent from external sources. In detail the project addresses the strong coupling between reactive flows, thermal environment, and structure loads. Therefore, the project is split into the main work packages combustion chamber, thrust nozzle, thrust chamber wall cooling, and test facilities. The highlights of the achieved progress in these work packages are described in the present publication.

Item URL in elib:https://elib.dlr.de/130214/
Document Type:Conference or Workshop Item (Speech)
Title:DLR Project TAUROS: TAU for Rocket Thrust Chamber Simulation
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Schneider, DirkUNSPECIFIEDhttps://orcid.org/0000-0002-4785-4244
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261
Martin, JanUNSPECIFIEDhttps://orcid.org/0000-0002-5050-2506
Stark, RalfUNSPECIFIEDhttps://orcid.org/0000-0003-1923-1901
Suslov, DmitryUNSPECIFIEDhttps://orcid.org/0000-0002-5160-9292
Tonti, FedericaUNSPECIFIEDhttps://orcid.org/0000-0002-2797-349X
Van Schyndel, JanUNSPECIFIEDhttps://orcid.org/0000-0002-4190-0377
Zhukov, Victor / V. P.UNSPECIFIEDhttps://orcid.org/0000-0003-0110-7419
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825
Costa Ruiz, EugeniUNSPECIFIEDhttps://orcid.org/0000-0002-0659-4167
Fechter, StefanUNSPECIFIEDhttps://orcid.org/0000-0001-5683-4715
Horchler, TimUNSPECIFIEDhttps://orcid.org/0000-0002-8439-8786
Karl, SebastianUNSPECIFIEDhttps://orcid.org/0000-0002-5558-6673
Hannemann, KlausUNSPECIFIEDhttps://orcid.org/0000-0002-9653-4087
Jack, SebastianUNSPECIFIEDhttps://orcid.org/0000-0002-1554-6503
Eggers, ThinoUNSPECIFIEDhttps://orcid.org/0000-0002-4377-7739
Lechtenberg, AnsgarUNSPECIFIEDhttps://orcid.org/0000-0003-4745-6921
Journal or Publication Title:Proceedings of the 8th European Conference for Aeronautics and Space Sciences
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
Keywords:rocket thrust chamber Simulation
Event Title:8th European Conference for Aeronautics and Space Sciences EUCASS
Event Location:Madrid, Spain
Event Type:international Conference
Event Dates:1. - 4. Jul. 2019
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 TAUROS (TAU for Rocket Thrust Chamber Simulation)
Location: Braunschweig , Göttingen , Lampoldshausen , Stuttgart
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Institute for Aerodynamics and Flow Technology > Spacecraft, BS
Institute of Combustion Technology > Computer Simulation
Institute of Space Propulsion > Rocket Propulsion
Institute of Space Propulsion > Engineering
Deposited By: Hanke, Michaela
Deposited On:18 Nov 2019 08:48
Last Modified:28 Mar 2023 11:02

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