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1. Although the acronym H2RG refers only to the readout integrated circuit, here we follow convention in the astronomical community and use it to refer to the complete hybrid detector array.
2. J. P. Gardner, J. C. Mather, M. Clampin, R. Doyon, M. A. Greenhouse, H. B. Hammel, J. B. Hutchings, P. Jakobsen, S. J. Lilly, K. S. Long, J. I. Lunine, M. J. McCaughrean, M. Mountain, J. Nella, G. H. Rieke, M. J. Rieke, H.-W. Rix, E. P. Smith, G. Sonneborn, M. Stiavelli, H. S. Stockman, R. A. Windhorst, and G. S. Wright, “The James Webb Space Telescope,” Space Sci. Rev. 123, 485606 (Apr. 2006), arXiv:astro-ph/0606175.
3. Matthew A. Greenhouse, Vicki Balzano, Pamela Davila, Michael P. Drury, Jamie L. Dunn, Stuart D. Glazer, Ed Greville, Gregory Henegar, Eric L. Johnson, Ray Lundquist, John C. Mccloskey, Raymond G. Ohl, Robert A. Rashford, and Mark F. Voyton, “Status of the james webb space telescope integrated science instrument module system,” UV/Optical/IR Space Telescopes and Instruments: Innovative Technologies and Concepts V. Edited by Tsakalakos 8146, 262 (Sep 2011),
4. The processed detector wafers are evaluated by current-voltage and optical testing of PECs. PECs are lithographically patterned adjacent to the main array(s) on the wafers, and are diced and wirebonded into leadless chip carrier (LCC) packages for cryogenic testing. They contain variable sized photodiodes, small test arrays, contact measurement structures, and other test devices used for evaluating the diode performance (dark current, quantum efficiency, contact resistance) and materials properties (diffusion length, carrier lifetime, etc.) for each processed wafer.
5. Markus Loose, James Beletic, James Garnett, and Min Xu, “High-performance focal plane arrays based on the hawaii-2rg/4g and the sidecar asic,” Focal Plane Arrays for Space Telescopes III. Edited by Grycewicz 6690, 10 (Sep 2007),
6. Markus Loose, Mark C. Farris, James D. Garnett, Donald N. B. Hall, and Lester J. Kozlowski, “Hawaii-2rg: a 2k × 2k cmos multiplexer for low and high background astronomy applications,” IR Space Telescopes and Instruments. Edited by John C. Mather. Proceedings of the SPIE 4850, 867 (Mar 2003),
7. S. H. Moseley, Richard G. Arendt, D. J. Fixsen, Don Lindler, Markus Loose, and Bernard J. Rauscher, “Reducing the read noise of h2rg detector arrays: eliminating correlated noise with efficient use of reference signals,” High Energy 7742, 36 (Jul 2010),
8. Bernard J. Rauscher, Richard G. Arendt, D. J. Fixen, Matthew Lander, Don Lindler, Markus Loose, S. H. Moseley, Donna V. Wilson, and Christos Xenophontos, “Reducing the read noise of hawaii-2rg based detector systems with improved reference sampling and subtraction (irs2),” Infrared Sensors 8155, 45 (Sep 2011),
9. J. E. Jellison, “Gold-indium intermetallic compounds: Properties and growth rates,” NASA Document, 145 (1979),
10. G. W. Powell and J. D. Braun, “Diffusion in the gold-indium system,” Trans. AIME 230, 694699 (Jun 1964).
11. B. J. Rauscher, O. Fox, P. Ferruit, R. J. Hill, A. Waczynski, Y. Wen, W. Xia-Serafino, B. Mott, D. Alexander, C. K. Brambora, R. Derro, C. Engler, M. B. Garrison, T. Johnson, S. S. Manthripragada, J. M. Marsh, C. Marshall, R. J. Martineau, K. B. Shakoorzadeh, D. Wilson, W. D. Roher, M. Smith, C. Cabelli, J. Garnett, M. Loose, S. Wong-Anglin, M. Zandian, E. Cheng, T. Ellis, B. Howe, M. Jurado, G. Lee, J. Nieznanski, P. Wallis, J. York, M. W. Regan, D. N. B. Hall, K. W. Hodapp, T. Böker, G. De Marchi, P. Jakobsen, and P. Strada, “Detectors for the James Webb Space Telescope Near-Infrared Spectrograph. I. Readout Mode, Noise Model, and Calibration Considerations,” PASP 119, 768786 (Jul. 2007), arXiv:0706.2344.
12. Carl Stahle, et al., “JWST-RPT-017457: Executive summary: Root cause determination,” NASA Document, 110 (Apr 2011),
13. Carl Stahle, et al., “JWST-RPT-017774: Executive summary 2d: Define tests to determine whether the existing detectors are qualified for flight,” NASA Document, 16 (Jul 2011),
14. James Beletic, et al., Proc SPIE in press (2012).
15. D. Brent Mott, Augustyn Waczynski, Yiting Wen, Bernard J. Rauscher, Nicholas Boehm, Meng P. Chiao, Lantrinh Degumbia, Greg Delo, Roger Foltz, Emily Kan, David Alexander, Craig Cabelli, Brian Clemons, Joseph Connelly, Alex Dea, Rebecca Derro, Charles Engler, Ali Feizi, Ori Fox, Robert J. Hill, Thomas E. Johnson, Matthew Lander, Don J. Lindler, Markus Loose, Sridhar S. Manthripragada, Kevin Novo-Gradac, Wayne D. Roher, Robert Rosenberry, Kamdin Shakoorzadeh, Miles T. Smith, Donna Wilson, and Joseph Zino, “Characterization of the detector subsystem for the near-infrared spectrograph (nirspec) on the james webb space telescope,” High Energy 7021, 66 (Aug 2008),

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The James Webb Space Telescope (JWST) is the successor to the Hubble Space Telescope. JWST will be an infrared-optimized telescope, with an approximately 6.5 m diameter primary mirror, that is located at the Sun-Earth L2 Lagrange point. Three of JWST’s four science instruments use Teledyne HgCdTe HAWAII-2RG (H2RG) near infrared detector arrays. During 2010, the JWST Project noticed that a few of its 5 μm cutoff H2RG detectors were degrading during room temperature storage, and NASA chartered a “Detector Degradation Failure Review Board” (DD-FRB) to investigate. The DD-FRB determined that the root cause was a design flaw that allowed indium to interdiffuse with the gold contacts and migrate into the HgCdTe detector layer. Fortunately, Teledyne already had an improved design that eliminated this degradation mechanism. During early 2012, the improved H2RG design was qualified for flight and JWST began making additional H2RGs. In this article, we present the two public DD-FRB “Executive Summaries” that: (1) determined the root cause of the detector degradation and (2) defined tests to determine whether the existing detectors are qualified for flight. We supplement these with a brief introduction to H2RG detector arrays, some recent measurements showing that the performance of the improved design meets JWST requirements, and a discussion of how the JWST Project is using cryogenic storage to retard the degradation rate of the existing flight spare H2RGs.


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