Analysing single event upsets in low Earth orbit considering the geomagnetic field.
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| Title: | Analysing single event upsets in low Earth orbit considering the geomagnetic field. |
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| Authors: | Zink, Julia1 (AUTHOR) julia.zink@irs.uni-stuttgart.de, Nöldeke, Christoph M.1 (AUTHOR) christoph.noeldeke@f06.uni-stuttgart.de, Gaißer, Steffen1 (AUTHOR) steffen.gaisser@irs.uni-stuttgart.de, Klinkner, Sabine1 (AUTHOR) klinkner@irs.uni-stuttgart.de |
| Source: | Advances in Space Research. May2026, Vol. 77 Issue 10, p10520-10528. 9p. |
| Subjects: | Geomagnetism, Galactic cosmic rays, Radiation damage, Universität Stuttgart, Solar activity, Earth's orbit, Space environment |
| Abstract: | The Flying Laptop small satellite, developed, built, and operated by the University of Stuttgart's Institute of Space Systems, has been operational in Low Earth Orbit (LEO) since July 2017. Throughout its mission, the satellite has experienced several Single Event Upsets (SEUs) in onboard electronic components. This research investigates the frequency of SEUs between 15 August 2017 and 28 May 2024 in the satellite's Static Random-Access Memory (SRAM) in relation to the satellite's position, the corresponding McIlwain parameter (L-value) and the vertical cutoff rigidity. The analysis revealed that SEU occurrences increase significantly with increasing L-value and in areas with low cutoff rigidities. Additionally, the data indicates a noteworthy variation in SEU frequency in relation to the solar activity. The frequency of SEUs declines as solar activity increases. This inverse relationship corresponds to the declining flux of Galactic Cosmic Rays (GCR) during periods of higher solar activity, indicating that most SEUs are caused by GCR rather than by Solar Energetic Particles (SEPs). This research provides insights into the impact of space weather on satellites in LEO. This knowledge is crucial to mitigate severe space weather induced system failures or anomalies, which in turn can increase a spacecraft's lifetime. This paper is a follow-up to the earlier work Noeldeke et al. (2021) , providing additional insights after more than seven years of satellite operation. [ABSTRACT FROM AUTHOR] |
| Copyright of Advances in Space Research is the property of Pergamon Press - An Imprint of Elsevier Science and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) | |
| Database: | Engineering Source |
| FullText | Text: Availability: 0 |
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| Header | DbId: egs DbLabel: Engineering Source An: 193312417 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: Analysing single event upsets in low Earth orbit considering the geomagnetic field. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Zink%2C+Julia%22">Zink, Julia</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> julia.zink@irs.uni-stuttgart.de</i><br /><searchLink fieldCode="AR" term="%22Nöldeke%2C+Christoph+M%2E%22">Nöldeke, Christoph M.</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> christoph.noeldeke@f06.uni-stuttgart.de</i><br /><searchLink fieldCode="AR" term="%22Gaißer%2C+Steffen%22">Gaißer, Steffen</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> steffen.gaisser@irs.uni-stuttgart.de</i><br /><searchLink fieldCode="AR" term="%22Klinkner%2C+Sabine%22">Klinkner, Sabine</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> klinkner@irs.uni-stuttgart.de</i> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22Advances+in+Space+Research%22">Advances in Space Research</searchLink>. May2026, Vol. 77 Issue 10, p10520-10528. 9p. – Name: Subject Label: Subjects Group: Su Data: <searchLink fieldCode="DE" term="%22Geomagnetism%22">Geomagnetism</searchLink><br /><searchLink fieldCode="DE" term="%22Galactic+cosmic+rays%22">Galactic cosmic rays</searchLink><br /><searchLink fieldCode="DE" term="%22Radiation+damage%22">Radiation damage</searchLink><br /><searchLink fieldCode="DE" term="%22Universität+Stuttgart%22">Universität Stuttgart</searchLink><br /><searchLink fieldCode="DE" term="%22Solar+activity%22">Solar activity</searchLink><br /><searchLink fieldCode="DE" term="%22Earth's+orbit%22">Earth's orbit</searchLink><br /><searchLink fieldCode="DE" term="%22Space+environment%22">Space environment</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: The Flying Laptop small satellite, developed, built, and operated by the University of Stuttgart's Institute of Space Systems, has been operational in Low Earth Orbit (LEO) since July 2017. Throughout its mission, the satellite has experienced several Single Event Upsets (SEUs) in onboard electronic components. This research investigates the frequency of SEUs between 15 August 2017 and 28 May 2024 in the satellite's Static Random-Access Memory (SRAM) in relation to the satellite's position, the corresponding McIlwain parameter (L-value) and the vertical cutoff rigidity. The analysis revealed that SEU occurrences increase significantly with increasing L-value and in areas with low cutoff rigidities. Additionally, the data indicates a noteworthy variation in SEU frequency in relation to the solar activity. The frequency of SEUs declines as solar activity increases. This inverse relationship corresponds to the declining flux of Galactic Cosmic Rays (GCR) during periods of higher solar activity, indicating that most SEUs are caused by GCR rather than by Solar Energetic Particles (SEPs). This research provides insights into the impact of space weather on satellites in LEO. This knowledge is crucial to mitigate severe space weather induced system failures or anomalies, which in turn can increase a spacecraft's lifetime. This paper is a follow-up to the earlier work Noeldeke et al. (2021) , providing additional insights after more than seven years of satellite operation. [ABSTRACT FROM AUTHOR] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of Advances in Space Research is the property of Pergamon Press - An Imprint of Elsevier Science and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.) |
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| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.1016/j.asr.2026.03.051 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 9 StartPage: 10520 Subjects: – SubjectFull: Geomagnetism Type: general – SubjectFull: Galactic cosmic rays Type: general – SubjectFull: Radiation damage Type: general – SubjectFull: Universität Stuttgart Type: general – SubjectFull: Solar activity Type: general – SubjectFull: Earth's orbit Type: general – SubjectFull: Space environment Type: general Titles: – TitleFull: Analysing single event upsets in low Earth orbit considering the geomagnetic field. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Zink, Julia – PersonEntity: Name: NameFull: Nöldeke, Christoph M. – PersonEntity: Name: NameFull: Gaißer, Steffen – PersonEntity: Name: NameFull: Klinkner, Sabine IsPartOfRelationships: – BibEntity: Dates: – D: 15 M: 05 Text: May2026 Type: published Y: 2026 Identifiers: – Type: issn-print Value: 02731177 Numbering: – Type: volume Value: 77 – Type: issue Value: 10 Titles: – TitleFull: Advances in Space Research Type: main |
| ResultId | 1 |