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
Referencia bibliográfica
Proceedings of the SPIE, Volume 9143, id. 91430K 14 pp. (2014).
Fecha de publicación:
8
2014
Número de citas
12
Número de citas referidas
8
Descripción
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.