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Modeling a Xenon Tank, its Heat Convection and In-Orbit Behavior with a 2D CFD Method

Merkel, Alexander (2019) Modeling a Xenon Tank, its Heat Convection and In-Orbit Behavior with a 2D CFD Method. Master's, RWTH Aachen.

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Xenon becomes increasingly important as a propellant for spacecrafts. As part of the development process, the thermal control of the tank during the loading and unloading procedure has to be designed. To aid in this task, a 2D model of xenon inside its tank during the pressurization and depressurization process, specifically for a zero-g environment, has been created using OpenFOAM. The physical theory behind fluid flows as well as the methodology the model creation is based upon and the used numerical settings are presented. The model was applied to compute the fluid properties and heat flow during xenon loading and unloading for the ESPRIT project. When comparing the results to 0D/1D simulations performed by EcosimPro and an internal Excel tool, phenomena not modeled with these approaches could be observed in the OpenFOAM results. This makes it a valuable addition to the tools available during the design of the propulsion system.

Item URL in elib:https://elib.dlr.de/140917/
Document Type:Thesis (Master's)
Title:Modeling a Xenon Tank, its Heat Convection and In-Orbit Behavior with a 2D CFD Method
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Merkel, AlexanderInstitut für Strahlantriebe und Turbomaschinen, RWTH Aachen, DUNSPECIFIEDUNSPECIFIED
Refereed publication:No
Open Access:Yes
Number of Pages:86
Keywords:xenon tank, electric propulsion, pressurization, OpenFOAM, zero-g environment, computational fluid dynamics
Institution:RWTH Aachen
Department:Institut für Strahlantriebe und Turbomaschinen
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:12 Feb 2021 07:45
Last Modified:12 Feb 2021 07:45

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