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24 April 2024 |
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The Mid-Infrared Instrument for JWST, II: Design and Build | G. S. Wright
; David Wright
; G. B. Goodson
; G. H. Rieke
; Gabby Aitink-Kroes
; J. Amiaux
; Ana Aricha-Yanguas
; Ruyman Azzolini
; Kimberly Banks
; D. Barrado-Navascues
; T. Belenguer-Davila
; J. A. D. L. Bloemmart
; Patrice Bouchet
; B. R. Brandl
; L. Colina
; Ors Detre
; Eva Diaz-Catala
; Paul Eccleston
; Scott D. Friedman
; Macarena Garcia-Marin
; Manuel Guedel
; Alistair Glasse
; Adrian M. Glauser
; T. P. Greene
; Uli Groezinger
; Tim Grundy
; Peter Hastings
; Th. Henning
; Ralph Hofferbert
; Faye Hunter
; N. C. Jessen
; K. Justtanont
; Avinash R. Karnik
; Mori A. Khorrami
; Oliver Krause
; Alvaro Labiano
; P.-O. Lagage
; Ulrich Langer
; Dietrich Lemke
; Tanya Lim
; Jose Lorenzo-Alvarez
; Emmanuel Mazy
; Norman McGowan
; M. E. Meixner
; Nigel Morris
; Jane E. Morrison
; Friedrich Mueller
; H.-U. Norgaard-Nielson
; Goeran Olofsson
; Brian O'Sullivan
; J.-W. Pel
; Konstantin Penanen
; M. B. Petach
; J. P. Pye
; T. P. Ray
; Etienne Renotte
; Ian Renouf
; M. E. Ressler
; Piyal Samara-Ratna
; Silvia Scheithauer
; Analyn Schneider
; Bryan Shaughnessy
; Tim Stevenson
; Kalyani Sukhatme
; Bruce Swinyard
; Jon Sykes
; John Thatcher
; Tuomo Tikkanen
; E. F. van Dishoeck
; C. Waelkens
; Helen Walker
; Martyn Wells
; Alex Zhender
; | Date: |
10 Aug 2015 | Abstract: | The Mid-InfraRed Instrument (MIRI) on the James Webb Space Telescope (JWST)
provides measurements over the wavelength range 5 to 28.5 microns. 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. | Source: | arXiv, 1508.2333 | Services: | Forum | Review | PDF | Favorites |
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