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Development and Design of a LOX/LNG Thrust Chamber by using Computer-Aided Optimization Methods

Haemisch, Jan and Suslov, Dmitry and Deeken, Jan C. (2023) Development and Design of a LOX/LNG Thrust Chamber by using Computer-Aided Optimization Methods. International Heat Transfer Conference, 2023-08-14 - 2023-08-18, Kapstadt, Südafrika. (In Press)

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The regenerative cooling still is one of the most crucial parts in designing a liquid rocket engine. The goal of an effective design is a trade-off between a sufficient cooling of the structure and a low pressure drop in the cooling channels. For an expander type cycle a third requirement arises: A sufficient enthalpy increase of the cooling fluid for the turbopumps to operate effectively. To prevent the combustion chamber from melting, the regenerative cooling has to be designed with a sufficient margin to respect all uncertainties. In this paper, the design of the regenerative cooling system will be described. A numerical method is used to optimize CFD simulations in order to reach all goals.

Item URL in elib:https://elib.dlr.de/199070/
Document Type:Conference or Workshop Item (Poster)
Title:Development and Design of a LOX/LNG Thrust Chamber by using Computer-Aided Optimization Methods
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Haemisch, JanUNSPECIFIEDhttps://orcid.org/0000-0001-9463-1740UNSPECIFIED
Suslov, DmitryUNSPECIFIEDhttps://orcid.org/0000-0002-5160-9292UNSPECIFIED
Deeken, Jan C.UNSPECIFIEDhttps://orcid.org/0000-0002-5714-8845UNSPECIFIED
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Status:In Press
Keywords:regenerative cooling, cryogenic rocket engines, optimization, cooling channels, heat transfer deterioration, HTD, LUMEN
Event Title:International Heat Transfer Conference
Event Location:Kapstadt, Südafrika
Event Type:international Conference
Event Start Date:14 August 2023
Event End Date:18 August 2023
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 LUMEN (Liquid Upper Stage Demonstrator Engine)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Applied Hydrogen Technologies
Institute of Space Propulsion > Rocket Engine Systems
Deposited By: Haemisch, Jan
Deposited On:11 Dec 2023 08:09
Last Modified:24 Apr 2024 20:59

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