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@INPROCEEDINGS{Neubert:862636,
      author       = {Neubert, Tom and Rongen, Heinz and Zimmermann, Egon and
                      Kaufmann, Martin and Olschewski, Friedhelm and van Waasen,
                      Stefan},
      title        = {{A} {L}ong-{L}ife {S}cience {S}ensor {E}lectronics for
                      {A}tmospheric {R}emote {S}ensing {I}maging from {C}ube{S}ats
                      in {L}ow-{E}arth-{O}rbits},
      reportid     = {FZJ-2019-02898},
      year         = {2019},
      abstract     = {CubeSats have become very popular in the past decades which
                      yields to a continuously increasing number of developers in
                      the academic field. For all science missions, customized
                      payload electronics have to be developed, depending on
                      measurement tasks and requirements. Especially for the
                      deployment of more complex remote sensing payloads,
                      state-of-the-art performance is needed to provide
                      operational control and specific data processing of the
                      image sensors. With a highly integrated System on Module
                      (SoM) architecture low resource requirements for both, power
                      and mass, but moderate to high processing power capabilities
                      are available. The major advantages are flexibility,
                      (re)programmability, modularity and module re-use in respect
                      to lower development time and costs. However, it is a
                      challenge to make this module suitable to implement it into
                      space environment. With an efficient approach a radiation
                      tolerant characteristics will be achieved by modelling the
                      radiation environment, estimating the hazards at module
                      level and reducing it to acceptable risks with necessary
                      measures of mitigation techniques. This approach results
                      into a sensor electronics which combines hardware and
                      software redundancies to assure system availability and
                      reliability for long life science missions in
                      Low-Earth-Orbits (LEO). An dual imager electronics design is
                      presented which uses module architecture based on
                      reconfigurable hardware with a processing unit as high
                      integrated commercial-off-the-shelf (COTS) components
                      integrated in a 6U 3U CubeSat. First qualification and
                      acceptance tests with the electronics will be shown.},
      month         = {Apr},
      date          = {2019-04-07},
      organization  = {EGU General Assembly 2019, Vienna
                       (Austria), 7 Apr 2019 - 12 Apr 2019},
      subtyp        = {After Call},
      cin          = {ZEA-2 / IEK-7},
      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)24},
      url          = {https://juser.fz-juelich.de/record/862636},
}