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  <controlfield tag="001">7238</controlfield>
  <controlfield tag="005">20250106135545.0</controlfield>
  <datafield tag="024" ind1="7" ind2=" ">
    <subfield code="a">10.1117/12.3017992</subfield>
    <subfield code="2">DOI</subfield>
  </datafield>
  <datafield tag="037" ind1=" " ind2=" ">
    <subfield code="a">SCART-2025-0015</subfield>
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  <datafield tag="100" ind1=" " ind2=" ">
    <subfield code="a">Yerlès, Matéo</subfield>
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  <datafield tag="245" ind1=" " ind2=" ">
    <subfield code="a">Cubesat multispectral space-based imaging spectrometer enhancing climate change monitoring</subfield>
  </datafield>
  <datafield tag="260" ind1=" " ind2=" ">
    <subfield code="c">2024</subfield>
  </datafield>
  <datafield tag="520" ind1=" " ind2=" ">
    <subfield code="a">Space-based spectrometers are of high importance for Earth observation and greenhouse gas sensing. We present a novel freeform pushbroom imaging spectrometer, covering the visible (400 - 1100 nm), near-infrared (1100 - 1700 nm) and thermal (8 - 14 mu m) wavelength range, showing a full field-of-view of 120 degrees, while fitting within a single CubeSat Unit. The design is composed of a freeform 2-mirror telescope, followed by a freeform spectrometer unit. The freeform telescope guides the light to the spectrometer entrance slit, after which a collimating mirror is present, and the light is split to the 3 spectrometer channels. Each spectrometer channel focuses the light onto a 2D detector providing both spatial and spectral information. The visible spectrometer channel comprises a transmission diffraction grating followed by 2 freeform mirrors, enabling a nadir spatial resolution of 9.87 km and a spectral resolution of 5.18 nm. The near-infrared and thermal spectrometer each comprise a reflective diffraction grating and 2 freeform mirrors, featuring a nadir spatial resolution of 4.13 km and 9.31 km, and a spectral resolution of 2.74 nm and 48.27 nm, respectively. All mirrors are described using XY polynomials, up to the 4th order, enabling a close to diffraction-limited performance. Consequently, this design might benefit future space missions enabling an improved Earth observation and climate monitoring.</subfield>
  </datafield>
  <datafield tag="594" ind1=" " ind2=" ">
    <subfield code="a">NO</subfield>
  </datafield>
  <datafield tag="700" ind1=" " ind2=" ">
    <subfield code="a">Schifano, Luca</subfield>
  </datafield>
  <datafield tag="700" ind1=" " ind2=" ">
    <subfield code="a">Dewitte, Steven</subfield>
  </datafield>
  <datafield tag="700" ind1=" " ind2=" ">
    <subfield code="a">Thienpont, Hugo</subfield>
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  <datafield tag="700" ind1=" " ind2=" ">
    <subfield code="a">Smeesters, Lien</subfield>
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  <datafield tag="773" ind1=" " ind2=" ">
    <subfield code="p">SPIE</subfield>
    <subfield code="v">13019</subfield>
    <subfield code="c">206-211</subfield>
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  <datafield tag="856" ind1="0" ind2=" ">
    <subfield code="f">steven.dewitte@ksb-orb.be</subfield>
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  <datafield tag="905" ind1=" " ind2=" ">
    <subfield code="a">published in</subfield>
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  <datafield tag="980" ind1=" " ind2=" ">
    <subfield code="a">REFERD</subfield>
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