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@ARTICLE{Neubert:864090,
      author       = {Neubert, Tom and Rongen, Heinz and Fröhlich, Denis and
                      Schardt, Georg and Dick, Markus and Nysten, Tobias and
                      Zimmermann, Egon and Kaufmann, Martin and Olschewski,
                      Friedhelm and van Waasen, Stefan},
      title        = {{S}ystem-on-module-based long-life electronics for remote
                      sensing imaging with {C}ube{S}ats in low-earth-orbits},
      journal      = {Journal of applied remote sensing},
      volume       = {13},
      number       = {03},
      issn         = {1931-3195},
      address      = {Bellingham Wash.},
      publisher    = {SPIE},
      reportid     = {FZJ-2019-03995},
      pages        = {032507},
      year         = {2019},
      abstract     = {CubeSats have become very popular science platforms in the
                      past decades, leading to a continuously increasing number of
                      developers in the academic field. For science missions,
                      customized payload electronics have to be developed,
                      depending on measurement tasks and requirements. Especially
                      for the deployment of complex remote sensing payloads,
                      state-of-the-art performance is needed to provide
                      operational control and specific data processing, e.g., for
                      image sensors. Highly integrated system-on-module (SoM)
                      architectures offer low resource requirements regarding
                      power and mass, but moderate to high processing power
                      capabilities. However, a requirement to use a standard SoM
                      in a satellite is to quantify its radiation tolerance. The
                      radiation environment has been modeled, estimating the
                      hazards at module level and reducing the risks to an
                      acceptable level by applying appropriate mitigation
                      techniques. This approach results in a sensor electronics
                      design that combines hardware and software redundancies to
                      assure system availability and reliability for long-life
                      science missions in low earth orbits. Integrated in a
                      miniaturized limb sounding instrument for atmospheric remote
                      sensing imaging, the payload electronics will be deployed on
                      a technology demonstration satellite for in-orbit
                      verification.},
      cin          = {ZEA-2 / IEK-7},
      ddc          = {620},
      cid          = {I:(DE-Juel1)ZEA-2-20090406 / I:(DE-Juel1)IEK-7-20101013},
      pnm          = {244 - Composition and dynamics of the upper troposphere and
                      middle atmosphere (POF3-244)},
      pid          = {G:(DE-HGF)POF3-244},
      typ          = {PUB:(DE-HGF)16},
      UT           = {WOS:000475321800001},
      doi          = {10.1117/1.JRS.13.032507},
      url          = {https://juser.fz-juelich.de/record/864090},
}