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  4. Lessons Learned and First Results of the E-Band CubeSat EIVE
 
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2025
Conference Paper
Title

Lessons Learned and First Results of the E-Band CubeSat EIVE

Abstract
A 6 Unit CubeSat was developed during the EIVE project to accommodate a challenging E-band transmitter payload. The system architecture of the EIVE CubeSat is introduced and recommendations for new designs are derived based on the lessons learned. The major part of experiences was gained from the on-board data handling and communication system, which includes SoCs and CCSDS protocol via S-band, the high-power electrical system’s design, the COTS attitude control system as well as the self-developed structure, mechanisms and harness. Moreover, first results and experiences with the subsystems and components during the LEOP are presented.
Author(s)
Koller, M.T.
University of Stuttgart
Bötsch-Zavrel, L.
University of Stuttgart
Eggert, M.
University of Stuttgart
Fugmann, M.
University of Stuttgart
Holeczek, C.
University of Stuttgart
Kranz, M.
University of Stuttgart
Lengowski, M.
University of Stuttgart
Löffler, T.
University of Stuttgart
Loidold, L.-M.
University of Stuttgart
Maier, P.
University of Stuttgart
Meier, J.
University of Stuttgart
Mohr, U.
University of Stuttgart
Müller, R.
University of Stuttgart
Pahler, A.
University of Stuttgart
Pätschke, S.
University of Stuttgart
Schweigert, R.
University of Stuttgart
Starzmann, D.
University of Stuttgart
Zietz, M.
University of Stuttgart
Haußmann, S.
University of Stuttgart
Manoliu, L.
University of Stuttgart
Schoch, B.
University of Stuttgart
Tessmann, Axel  
Fraunhofer-Institut für Angewandte Festkörperphysik IAF  
Henneberger, R.
Radiometer (Germany)
Freese, J.
Tesat-Spacecom (Germany)
Steinmetz, F.
Thales Alenia Space
Klinkner, S.
University of Stuttgart
Mainwork
Deutscher Luft- und Raumfahrtkongress 2023  
Project(s)
Exploratory In-Orbit Verification of an E/W-Band Satellite Communication Link
Funder
Deutsches Zentrum für Luft- und Raumfahrt e.V. -DLR-  
Conference
Deutscher Luft- und Raumfahrtkongress 2023  
DOI
10.25967/610298
Language
English
Fraunhofer-Institut für Angewandte Festkörperphysik IAF  
Keyword(s)
  • 6U CubeSat

  • Lessons Learned

  • Satellite Bus Design

  • Launch and Early Orbit Phase

  • Flight Results

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