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

G. S. Wright, David Wright, G. B. Goodson, G. H. Rieke, Gabby Aitink-Kroes, J. Amiaux, Ana Aricha-Yanguas, Ruyman Azzollini, Kimberly Banks, N. C. Jessen, H. U. Nørgaard-Nielsen

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Abstract

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 similar to 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.
Original languageEnglish
JournalPublications of the Astronomical Society of the Pacific
Volume127
Issue number953
Pages (from-to)595-611
ISSN0004-6280
DOIs
Publication statusPublished - 2015

Bibliographical note

For full list of authors, consult the publication

Keywords

  • Space vehicles: instruments
  • instrumentation: photometers
  • instrumentation: spectrographs

Cite this

Wright, G. S., Wright, D., Goodson, G. B., Rieke, G. H., Aitink-Kroes, G., Amiaux, J., Aricha-Yanguas, A., Azzollini, R., Banks, K., Jessen, N. C., & Nørgaard-Nielsen, H. U. (2015). The Mid-Infrared Instrument for the James Webb Space Telescope, II: Design and Build. Publications of the Astronomical Society of the Pacific, 127(953), 595-611. https://doi.org/10.1086/682253