Bibcode
Maciaszek, T.; Ealet, Anne; Jahnke, Knud; Prieto, Eric; Barbier, Rémi; Mellier, Yannick; Costille, Anne; Ducret, Franck; Fabron, Christophe; Gimenez, Jean-Luc; Grange, Robert; Martin, Laurent; Rossin, Christelle; Pamplona, Tony; Vola, Pascal; Clémens, Jean Claude; Smadja, Gérard; Amiaux, Jérome; Barrière, Jean Christophe; Berthe, Michel; De Rosa, Adriano; Franceschi, Enrico; Morgante, Gianluca; Trifoglio, Massimo; Valenziano, Luca; Bonoli, Carlotta; Bortoletto, Favio; D'Alessandro, Maurizio; Corcione, Leonardo; Ligori, Sebastiano; Garilli, Bianca; Riva, Marco; Grupp, Frank; Vogel, Carolin; Hormuth, Felix; Seidel, Gregor; Wachter, Stefanie; Diaz, J. J.; Grañena, Ferran; Padilla, Cristobal; Toledo, Rafael; Lilje, Per B.; Solheim, Bjarte G. B.; Toulouse-Aastrup, Corinne; Andersen, Michael; Holmes, Warren; Israelsson, Ulf; Seiffert, Michael; Weber, Carissa; Waczynski, Augustyn; Laureijs, René J.; Racca, Giuseppe; Salvignol, Jean-Christophe; Strada, Paolo
Bibliographical reference
Proceedings of the SPIE, Volume 9143, id. 91430K 14 pp. (2014).
Advertised on:
8
2014
Citations
15
Refereed citations
10
Description
The Euclid mission objective is to understand why the expansion of the
Universe is accelerating by mapping the geometry of the dark Universe by
investigating the distance-redshift relationship and tracing the
evolution of cosmic structures. The Euclid project is part of ESA's
Cosmic Vision program with its launch planned for 2020. The NISP (Near
Infrared Spectro-Photometer) is one of the two Euclid instruments and is
operating in the near-IR spectral region (0.9-2μm) as a photometer
and spectrometer. The instrument is composed of: - a cold (135K)
optomechanical subsystem consisting of a SiC structure, an optical
assembly (corrector and camera lens), a filter wheel mechanism, a grism
wheel mechanism, a calibration unit and a thermal control system - a
detection subsystem based on a mosaic of 16 Teledyne HAWAII2RG cooled to
95K with their front-end readout electronic cooled to 140K, integrated
on a mechanical focal plane structure made with Molybdenum and Aluminum.
The detection subsystem is mounted on the optomechanical subsystem
structure - a warm electronic subsystem (280K) 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 presentation
describes the architecture of the instrument at the end of the phase B
(Preliminary Design Review), the expected performance, the technological
key challenges and preliminary test results obtained on a detection
system demonstration model.