Ferrofluid reaction wheel development and in-orbit verification

dc.contributor.authorEhresmann, Manfred
dc.contributor.authorZajonz, Sebastian
dc.contributor.authorKorn, Christian
dc.contributor.authorGroßmann, Steffen
dc.contributor.authorDietrich, Janoah
dc.contributor.authorKob, Maximilian
dc.contributor.authorPhilipp, Daniel
dc.contributor.authorTurco, Fabrizio
dc.contributor.authorSteinert, Michael
dc.contributor.authorO’Donohue, Michael
dc.contributor.authorHeinz, Nicolas
dc.contributor.authorGutierrez, Elizabeth
dc.contributor.authorWagner, Alexander
dc.contributor.authorBölke, Daniel
dc.contributor.authorSütterlin, Saskia
dc.contributor.authorSchneider, Maximilian
dc.contributor.authorRemane, Yolantha
dc.contributor.authorKreul, Phil
dc.contributor.authorWank, Bianca
dc.contributor.authorBuchfink, Manuel
dc.contributor.authorAcker, Denis
dc.contributor.authorHofmann, Sonja
dc.contributor.authorKarahan, Bahar
dc.contributor.authorRuffner, Silas
dc.contributor.authorSchäfer, Felix
dc.contributor.authorHerdrich, Georg
dc.date.accessioned2025-10-30T10:32:34Z
dc.date.issued2025
dc.date.updated2025-10-28T01:14:09Z
dc.description.abstractIn contemporary satellite systems, the Attitude and Orbit Control System (AOCS) manages internal torque generation primarily through Reaction Wheels (RW) and Control Moment Gyros (CMG), which use mechanically mounted rotating disks to control orientation without expelling mass. Unlike magnetorquers, which interact with Earth’s magnetic field, or thruster-based Reaction Control Systems (RCS), which generate external forces by expelling propellant, RW and CMG systems rely solely on momentum exchange within the spacecraft. While state-of-the-art RWs are highly reliable and have demonstrated exceptional performance over decades of operation, their design still presents inherent challenges, such as wear, nonlinear friction effects, and tribological degradation of contact surfaces. These challenges are critical in space, where repairs are impractical and/or resource-intense. Consequently, engineers have devoted significant effort to developing robust and reliable mechanical reaction wheels. This paper explores an innovative proof-of-concept design based on a fluid-magnetic system utilizing ferrofluids and permanent magnets. This study aims to address limitations of traditional RWs by eliminating mechanical interfaces susceptible to wear and tear and replacing them with a low friction ferrofluidic bearing. Ferrofluid-based system concepts can offer a longer life due to reduced wear and tear, lower production costs by requiring less exotic materials and tolerances, self-center within the provided magnetic potential field and can therefore exhibit reduced vibration behavior. The Ferrowheel experiment, flown as part of the FARGO mission ( Überflieger 2 competition of the space agency within DLR) in March and April 2023, demonstrated the feasibility of ferrofluidic bearings for attitude control in ISS microgravity. These results contribute to exploration of innovative reaction wheel technologies, highlighting the potential of fluid-based systems for applications requiring enhanced robustness and reduced mechanical wear.en
dc.description.sponsorshipProjekt DEAL
dc.description.sponsorshipGerman space agency within DLR
dc.identifier.issn1868-2510
dc.identifier.issn1868-2502
dc.identifier.other1940883814
dc.identifier.urihttp://nbn-resolving.de/urn:nbn:de:bsz:93-opus-ds-174030de
dc.identifier.urihttps://elib.uni-stuttgart.de/handle/11682/17403
dc.identifier.urihttps://doi.org/10.18419/opus-17384
dc.language.isoen
dc.relation.uridoi:10.1007/s12567-025-00601-2
dc.rightsCC BY
dc.rightsinfo:eu-repo/semantics/openAccess
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.subject.ddc620
dc.titleFerrofluid reaction wheel development and in-orbit verificationen
dc.typearticle
dc.type.versionpublishedVersion
ubs.fakultaetLuft- und Raumfahrttechnik und Geodäsie
ubs.institutInstitut für Raumfahrtsysteme
ubs.publikation.seiten917-929
ubs.publikation.sourceCEAS space journal 17 (2025), S. 917-929
ubs.publikation.typZeitschriftenartikel

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