Maciaszek , T , Ealet , A , Gillard , W , Jahnke , K , Barbier , R , Prieto , E , Bon , W , Bonnefoi , A , Jaquet , M , Martin , L , Sanchez , P , Auricchio , N , Franceschi , E , Medinaceli , E , Trifoglio , M , Corcione , L , Capobianco , V , Ligori , S , Dusini , S , Borsato , E , Lilje , P , Andersen , M , Andersen , J , Sorensen , A , Jessen , N ....
University of Copenhagen: Research / Forskning ved Københavns Universitet
نبذة مختصرة :
The NISP (Near Infrared Spectrometer and Photometer) is one of the two Euclid instruments (see ref [1]). It operates in the near-IR spectral region (950 -2020nm) as a photometer and spectrometer. The instrument is composed of: - a cold (135 K) optomechanical subsystem consisting of a Silicon carbide structure, an optical assembly, a filter wheel mechanism, a grism wheel mechanism, a calibration unit, and a thermal control system, - a detection system based on a mosaic of 16 H2RG with their front-end readout electronic, and - a warm electronic system (290 K) composed of a data processing / detector control unit and of an instrument control unit that interfaces with the spacecraft via a 1553 bus for command and control and via Spacewire links for science data. This paper presents: - the final architecture of the flight model instrument and subsystems, and - the performance and the ground calibration measurement done at NISP level and at Euclid Payload Module level at operational cold temperature.
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