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@INPROCEEDINGS{Kaufmann:1021459,
      author       = {Kaufmann, Martin and Chen, Qiuyu and Ntokas, Konstantin and
                      Ungermann, Jörn and Preusse, Peter and Ern, Manfred and
                      Olschewski, Friedhelm and Wroblowski, Oliver and Miebach,
                      Marco and Augspurger, Tobias and Neubert, Tom and
                      Offermanns, Guido and Riese, Martin and Chandran, Amal and
                      Eastes, Richard},
      title        = {{A} {SATELLITE} {INSTRUMENT} {TO} {STUDY} {MESOSPHERE}
                      {AND} {LOWER} {THERMOSPHERE} {WAVE} {DYNAMICS}},
      reportid     = {FZJ-2024-00752},
      year         = {2023},
      abstract     = {A novel limb sounder for the measurement of temperature at
                      the mesosphere and lower thermosphere boundary is presented.
                      The instrument is designed to fly on Micro- and
                      Nanosatelliteplatforms for the deployment in satellite
                      constellations. The goal is to obtain a dense, 4-dimensional
                      mesh of temperatures for resolving the small scale,
                      time-varying waves that coupleatmospheric regions.The
                      instrument’s core element is a spatial heterodyne
                      interferometer, which is a monolithicMichelson-type
                      interferometer, particularly suitable for harsh
                      environments. The instrumentsuccessfully completed a
                      student-led rocket mission and an in-orbit satellite
                      technology demonstration. Upcoming deployments are within an
                      international satellite program in research andeducation and
                      an in-orbit demonstration and validation mission of the
                      European Union. Thesemissions will improve the maturity of
                      the measurement concept based on extensive
                      in-orbitcharacterizations.A focus of this presentation is on
                      a two-satellite mission concept to obtain highly
                      resolvedgravity wave momentum fluxes, one of the key
                      quantities to understand the coupling betweenthe Earth
                      atmosphere and lower space. This is relevant to our
                      capabilities for near real-timespace weather prediction and
                      to improving space environment climatology.},
      month         = {Apr},
      date          = {2023-04-16},
      organization  = {5th COSPAR Symposium 2023, Singapore
                       (Singapore), 16 Apr 2023 - 21 Apr 2023},
      subtyp        = {After Call},
      cin          = {IEK-7 / ZEA-2 / ZEA-1},
      cid          = {I:(DE-Juel1)IEK-7-20101013 / I:(DE-Juel1)ZEA-2-20090406 /
                      I:(DE-Juel1)ZEA-1-20090406},
      pnm          = {2112 - Climate Feedbacks (POF4-211)},
      pid          = {G:(DE-HGF)POF4-2112},
      typ          = {PUB:(DE-HGF)6},
      url          = {https://juser.fz-juelich.de/record/1021459},
}