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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
Publications of the Astronomical Society of the Pacific, 07/2015, Letnik: 127, Številka: 953Journal Article
The Mid-InfraRed Instrument (MIRI) on the James Webb Space Telescope (JWST) provides measurements over the wavelength range 5 to 28.5 μm. 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.
