3.8 Proceedings Paper

Euclid Near Infrared Spectrometer and Photometer instrument flight model presentation, performance, and ground calibration results summary

Publisher

SPIE-INT SOC OPTICAL ENGINEERING
DOI: 10.1117/12.2630338

Keywords

Euclid; Spectroscopy; Photometry; Infrared; Instrument; NISP

Funding

  1. Academy of Finland
  2. Agenzia Spaziale Italiana
  3. Belgian Science Policy
  4. Canadian Euclid Consortium
  5. Centre National d'Etudes Spatiales
  6. Deutsches Zentrum fur Luft und Raumfahrt
  7. Danish Space Research Institute
  8. Fundacao para a Ciencia e a Tecnologia
  9. Ministerio de Economia y Competitividad
  10. National Aeronautics and Space Administration
  11. National Astronomical Observatory of Japan
  12. Netherlandse Onderzoekschool Voor Astronomie
  13. Norwegian Space Agency
  14. Romanian Space Agency
  15. State Secretariat for Education
  16. Research and Innovation (SERI) at the Swiss Space Office (SSO)
  17. United Kingdom Space Agency

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This paper presents the final architecture and subsystems of the NISP instrument, along with the performance and ground calibration measurements conducted at operational cold temperature.
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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