Euclid near infrared spectrometer and photometer instrument flight model presentation, performance, and ground calibration results summary
- Maciaszek, T.
- Ealet, A.
- Gillard, W.
- Jahnke, K.
- Barbier, R.
- Prieto, E.
- Bon, W.
- Bonnefoi, A.
- Caillat, A.
- Carle, M.
- Costille, A.
- Ducret, F.
- Fabron, C.
- Foulon, B.
- Gimenez, J.-L.
- Grassi, E.
- Jaquet, M.
- Le Mignant, D.
- Martin, L.
- Pamplona, T.
- Sanchez, P.
- Clémens, J.-C.
- Caillat, L.
- Niclas, M.
- Secroun, A.
- Kubik, B.
- Ferriol, S.
- Berthe, M.
- Barrière, J.-C.
- Fontignie, J.
- Valenziano, L.
- Auricchio, N.
- Battaglia, P.
- De Rosa, A.
- Farinelli, R.
- Franceschi, E.
- Medinaceli, E.
- Morgante, G.
- Sortino, F.
- Trifoglio, M.
- Corcione, L.
- Capobianco, V.
- Ligori, S.
- Dusini, S.
- Borsato, E.
- Dal Corso, F.
- Laudisio, F.
- Sirignano, C.
- Stanco, L.
- Ventura, S.
- Patrizii, L.
- Chiarusi, T.
- Fornari, F.
- Giacomini, F.
- Margiotta, A.
- Mauri, N.
- Pasqualini, L.
- Sirri, G.
- Spurio, M.
- Tenti, M.
- Travaglini, R.
- Bonoli, C.
- Bortoletto, F.
- Balestra, A.
- Dalessandro, M.
- Grupp, F.
- Penka, D.
- Steinwagner, J.
- Hormuth, F.
- Schirmer, M.
- Seidel, G.
- Padilla, C.
- Casas, R.
- Lloro, Y.
- Toledo-Moreo, R.
- Gomez, J.
- Colodro-Conde, C.
- Lizán, D.
- Diaz, J.-J.
- Lilje, P.
- Andersen, M.I.
- Andersen, J.
- Sørensen, A.N.
- Hornstrup, A.
- Jessen, N.C.
- Thizy, C.
- Holmes, W.
- Pniel, M.
- Jhabvala, M.
- Pravdo, S.
- Seiffert, M.
- Waczynski, A.
- Laureij, R.J.
- Racca, G.
- Salvignol, J.-C.
- Boenke, T.
- Strada, P.
- Mellier, Y.
DOIAbstract
International audienceThe 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 (135K) 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. - a warm electronic system (290K) 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 Sp...
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