دورية أكاديمية

TheMid-Infrared Instrument for the James Webb Space Telescope, II: Design and Build.

التفاصيل البيبلوغرافية
العنوان: TheMid-Infrared Instrument for the James Webb Space Telescope, II: Design and Build.
المؤلفون: 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
المصدر: Publications of the Astronomical Society of the Pacific; Jul2015, Vol. 127 Issue 953, p595-611, 17p
مصطلحات موضوعية: INFRARED equipment, ASTRONOMICAL spectroscopy, INTEGRAL field spectroscopy, WAVELENGTH measurement, FLIGHT (Aerodynamics)
الشركة/الكيان: JAMES Webb Space Telescope (Spacecraft)
مستخلص: 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. [ABSTRACT FROM AUTHOR]
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قاعدة البيانات: Complementary Index