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The Mid-Infrared Instrument for the James Webb Space Telescope, II: Design and Build

Authors :
Wright, G. S.
Wright, David
Goodson, G. B.
Rieke, G. H.
Aitink-Kroes, Gabby
Amiaux, J.
Aricha-Yanguas, Ana
Azzollini, Ruymán
Banks, Kimberly
Barrado-Navascues, D.
Belenguer-Davila, T.
Bloemmart, J. A. D. L.
Bouchet, Patrice
Brandl, B. R.
Colina, L.
Detre, Örs
Diaz-Catala, Eva
Eccleston, Paul
Friedman, Scott D.
García-Marín, Macarena
Güdel, Manuel
Glasse, Alistair
Glauser, Adrian M.
Greene, T. P.
Groezinger, Uli
Grundy, Tim
Hastings, Peter
Henning, Th.
Hofferbert, Ralph
Hunter, Faye
Jessen, N. C.
Justtanont, K.
Karnik, Avinash R.
Khorrami, Mori A.
Krause, Oliver
Labiano, Alvaro
Lagage, P.-O.
Langer, Ulrich
Lemke, Dietrich
Lim, Tanya
Lorenzo-Alvarez, Jose
Mazy, Emmanuel
McGowan, Norman
Meixner, M. E.
Morris, Nigel
Morrison, Jane E.
Müller, Friedrich
Nø rgaard-Nielson, H.-U.
Olofsson, Göran
O'Sullivan, Brian
Pel, J.-W.
Penanen, Konstantin
Petach, M. B.
Pye, J. P.
Ray, T. P.
Renotte, Etienne
Renouf, Ian
Ressler, M. E.
Samara-Ratna, Piyal
Scheithauer, Silvia
Schneider, Analyn
Shaughnessy, Bryan
Stevenson, Tim
Sukhatme, Kalyani
Swinyard, Bruce
Sykes, Jon
Thatcher, John
Tikkanen, Tuomo
van Dishoeck, E. F.
Waelkens, C.
Walker, Helen
Wells, Martyn
Zhender, Alex
Source :
Publications of the Astronomical Society of the Pacific; July 2015, Vol. 127 Issue: 953 p595-611, 17p
Publication Year :
2015

Abstract

The Mid-InfraRed Instrument (MIRI) on the James Webb Space Telescope(JWST) provides measurements over the wavelength range 5 to 28.5 ?m. MIRI has, within a single "package," four key scientific functions: photometric imaging, coronagraphy, single-source low-spectral resolving power (R ? 100) spectroscopy, and medium-resolving power (R ? 1500 to 3500) integral field spectroscopy. An associated cooler system maintains MIRI at its operating temperature of < 6.7 K. This paper describes the driving principles behind the design of MIRI, the primary design parameters, and their realization in terms of the "as-built" instrument. It also describes the test program that led to delivery of the tested and calibrated Flight Model to NASA in 2012, and the confirmation after delivery of the key interface requirements.

Details

Language :
English
ISSN :
00046280 and 15383873
Volume :
127
Issue :
953
Database :
Supplemental Index
Journal :
Publications of the Astronomical Society of the Pacific
Publication Type :
Periodical
Accession number :
ejs56699596
Full Text :
https://doi.org/10.1086/682253