elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Accessibility | Contact | Deutsch
Fontsize: [-] Text [+]

Dependency of Inner Liner Surface Temperature on Coolant Mass Flow Rate and Heat Flux in Rocket Combustion Chambers

Kringe, Pascal and Riccius, Jörg and Zametaev, E. and Oschwald, Michael and Gernoth, Andreas and Soller, Sebastian and Lehmann, Marcus and Reese, Stefanie (2021) Dependency of Inner Liner Surface Temperature on Coolant Mass Flow Rate and Heat Flux in Rocket Combustion Chambers. Space Propulsion 2020 + 1, 2021-03-17 - 2021-03-19, Online.

[img] PDF
859kB

Item URL in elib:https://elib.dlr.de/146265/
Document Type:Conference or Workshop Item (Speech)
Title:Dependency of Inner Liner Surface Temperature on Coolant Mass Flow Rate and Heat Flux in Rocket Combustion Chambers
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Kringe, PascalUNSPECIFIEDhttps://orcid.org/0000-0003-2866-8419UNSPECIFIED
Riccius, JörgUNSPECIFIEDhttps://orcid.org/0000-0002-5935-874XUNSPECIFIED
Zametaev, E.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825UNSPECIFIED
Gernoth, AndreasESA, ESTEC, Noordwijk, NiederlandeUNSPECIFIEDUNSPECIFIED
Soller, SebastianArianeGroup GmbH, Munich, GermanyUNSPECIFIEDUNSPECIFIED
Lehmann, MarcusArianeGroup GmbH, Munich, GermanyUNSPECIFIEDUNSPECIFIED
Reese, StefanieInstitute of Applied Mechanics, RWTH Aachen University, Aachen, GermanyUNSPECIFIEDUNSPECIFIED
Date:2021
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:liquid rocket engine combustion chamber, convective heat transfer, Nusselt number, high thermal conductivity copper
Event Title:Space Propulsion 2020 + 1
Event Location:Online
Event Type:international Conference
Event Start Date:17 March 2021
Event End Date:19 March 2021
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 - Reusable Space Systems and Propulsion Technology
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion Technology
Deposited By: Hanke, Michaela
Deposited On:01 Dec 2021 08:07
Last Modified:24 Apr 2024 20:45

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
OpenAIRE Validator logo electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.