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Dive into the research topics where Craig R. McCreight is active.

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Featured researches published by Craig R. McCreight.


Astrophysical Journal Supplement Series | 2004

The Infrared Array Camera (IRAC) for the Spitzer Space Telescope

Giovanni G. Fazio; Joseph L. Hora; Lori E. Allen; M. L. N. Ashby; Pauline Barmby; Lynne K. Deutsch; Jia-Sheng Huang; S. C. Kleiner; Massimo Marengo; S. T. Megeath; Gary J. Melnick; Michael Andrew Pahre; Brian M. Patten; J. Polizotti; H. A. Smith; R. S. Taylor; Zhong Wang; Steven P. Willner; William F. Hoffmann; Judith L. Pipher; William J. Forrest; C. W. McMurty; Craig R. McCreight; Mark E. McKelvey; Robert E. McMurray; David G. Koch; S. H. Moseley; Richard G. Arendt; John Eric Mentzell; Catherine T. Marx

The Infrared Array Camera (IRAC) is one of three focal plane instruments on the Spitzer Space Telescope. IRAC is a four-channel camera that obtains simultaneous broadband images at 3.6, 4.5, 5.8, and 8.0 � m. Two nearly adjacent 5A2 ; 5A2 fields of view in the focal plane are viewed by the four channels in pairs (3.6 and 5.8 � m; 4.5 and 8 � m). All four detector arrays in the camera are 256 ; 256 pixels in size, with the two shorter wavelength channels using InSb and the two longer wavelength channels using Si:As IBC detectors. IRAC is a powerful survey instrument because of its high sensitivity, large field of view, and four-color imaging. This paper summarizes the in-flight scientific, technical, and operational performance of IRAC.


Proceedings of SPIE | 2004

In-flight performance and calibration of the Infrared Array Camera (IRAC) for the Spitzer Space Telescope

Joseph L. Hora; Giovanni G. Fazio; Lori E. Allen; Matthew L. N. Ashby; Pauline Barmby; Lynne K. Deutsch; Jiasheng S. Huang; Massimo Marengo; S. T. Megeath; Gary J. Melnick; Michael Andrew Pahre; Brian M. Patten; H. A. Smith; Zhong Wang; Steven P. Willner; William F. Hoffmann; Judith L. Pipher; William J. Forrest; Craig W. McMurtry; Craig R. McCreight; Mark E. McKelvey; Robert E. McMurray; S. H. Moseley; Richard G. Arendt; John Eric Mentzell; Catherine T. Marx; Dale J. Fixsen; Eric V. Tollestrup; Peter R. M. Eisenhardt; Daniel Stern

The Infrared Array Camera (IRAC) is one of three focal plane instruments on board the Spitzer Space Telescope. IRAC is a four-channel camera that obtains simultaneous broad-band images at 3.6, 4.5, 5.8, and 8.0 μm in two nearly adjacent fields of view. We summarize here the in-flight scientific, technical, and operational performance of IRAC.


Astronomical Telescopes and Instrumentation | 2003

Large Format Si:As IBC Array Performance for NGST and Future IR Space Telescope Applications

Kimberly A. Ennico; Mark E. McKelvey; Craig R. McCreight; Robert E. McMurray; Roy R. Johnson; Alan W. Hoffman; Peter J. Love; Nancy A. Lum

A mid-infrared(5-30 micron) instrument aboard a cryogenic space telescope can have an enormous impact in resolving key questions in astronomy and cosmology. A space platforms greatly reduced thermal backgrounds (compared to airborne or ground-based platforms), allow for more sensitive observations of dusty young galaxies at high redshifts, star formation of solar-type stars in the local universe, and formation and evolution of planetary disks and systems. The previous generations largest, most sensitive infrared detectors at these wavelengths are 256 x 256 pixel Si:As impurity band conduction devices built by Raytheon Infrared Operations for the SIRTF/IRAC instrument. Raytheon has successfully enhanced these devices, increasing the pixel count by a factor of 16 while matching or exceeding SIRTF/IRAC device performance. NASA-Ames Research Center in collaboration with Raytheon has tested the first high performance large format (1024 x 1024) Si:As IBC arrays for low background applications, such as for the mid-IR instrument on NGST and future IR Explorer missions. These hybrid devices consist of radiation-hard SIRTF/IRAC-type Si:As IBC material mated to a readout multiplexer that has been specially processed for operation at low cryogenic temperatures (below 10 K), yielding high device sensitivity over a wavelength range of 5-28 microns. In this paper, we present laboratory test results from these benchmark devices. Continued development in this technology is essential for conducting large-area surveys of the local and early universe through observation and for complementing future missions such as NGST, TPF, and FIRST.


IEEE Transactions on Nuclear Science | 2005

Transient radiation effects in ultra-low noise HgCdTe IR detector arrays for space-based astronomy

James C. Pickel; Robert A. Reed; Ray Ladbury; Paul W. Marshall; Thomas M. Jordan; George Gee; Bryan Fodness; Mark E. McKelvey; Robert E. McMurray; Kim Ennico; Craig R. McCreight; Augustyn Waczynski; Elizabeth J. Polidan; Scott D. Johnson; Robert A. Weller; Marcus H. Mendenhall; Ronald D. Schrimpf

We present measurements of proton-induced single event transients in ultra-low noise HgCdTe IR detector arrays being developed for space-based astronomy and compare to modeling results.


Optical Science and Technology, SPIE's 48th Annual Meeting | 2004

Radiation environment performance of JWST prototype FPAs

Mark E. McKelvey; Kimberly A. Ennico; Roy R. Johnson; Paul W. Marshall; Robert E. McMurray; Craig R. McCreight; Jim C. Pickel; Robert A. Reed

As the logical extension of the 20-year mission of the Hubble Space Telescope, NASA plans to launch the James Webb Space Telescope (JWST, formerly NGST) near the end of this decade. As Hubbles scientific and technological successor, equipped with a 6-meter-class deployable mirror, JWST will allow observations of the very early universe and initial formation of galaxies at levels not achievable today. JWSTs unprecedented sensitivity cannot be utilized without a new class of IR focal plane arrays whose performance matches that of the telescope. In particular, JWST focal planes must be able to withstand the ionizing-particle radiation environment expected for its Lagrange-point (L2) orbit and ten-year mission lifetime goal. To help determine their suitability for JWST, NASA is evaluating prototype megapixel-class readouts and hybrid detector arrays under proton bombardment to simulate the anticipated JWST lifetime radiation dose. This report describes the results of early tests on devices from two manufacturers using photovoltaic (HgCdTe or InSb) candidate near-infrared detector structures. Results to date have shown encouraging performance, along with some areas of continuing concern.


Applied Optics | 1981

Infrared charge-injection-device array performance at low background.

Craig R. McCreight; John H. Goebel

Low-background tests of a 1 x 32 Si:Bi charge-injection-device (CID) IR detector array were carried out to evaluate its feasibility for space-based astronomical observations. Optimum performance was obtained at a temperature of 11 K. The device showed a peak responsivity of 4.4 A/W, an average noise level of ~670 electrons, and a minimum noise equivalent power of 3 x 10(-17) W/[equation] for 1-sec integration time. This sensitivity compares well with that of discrete extrinsic silicon photoconductors. The measured sensitivity, plus the apparent absence of anomalous effects, make extrinsic silicon CID arrays very promising for astronomical applications.


Optical Science and Technology, SPIE's 48th Annual Meeting | 2004

Orion II: the second-generation readout multiplexer for the largest infrared hybrid focal plane

Kenneth Michael Merrill; Albert M. Fowler; William J. Ball; Arne A. Henden; Fred Vrba; Craig R. McCreight

The Orion program developed a 2048x2048 infrared focal plane using InSb PV diodes for detectors. Several of these focal planes have been produced. However, the yield of the original readout multiplexer was not up to expectations owing to unanticipated shorts in the fabrication process. Since these shorts occurred at the metal 1-metal 2 crossover points and there are over 9 million such crossovers, the design had to be modified to work around these problems. Thus the Orion II readout was developed. The work is being done at the Raytheon Vision Systems (RVS) division (most recently Raytheon Infrared Operations, but better known as SBRC) by many of the same people who created the Orion I and ALADDIN focal planes. The design is very similar to the Orion I design with the addition of circuitry to work around the effect of the metal 1-metal 2 shorts. In this paper we will discuss the unique design features of this device as well as present test data taken from the new devices.


Infrared Technology and Applications XXIX | 2003

Development of Si:As impurity band conduction (IBC) detectors for mid-infrared applications

Ken J. Ando; Alan W. Hoffman; Peter J. Love; Andrew G. Toth; Conrad Anderson; George R. Chapman; Craig R. McCreight; Kimberly A. Ennico; Mark E. McKelvey; Robert E. McMurray

Si:As Impurity Band Conduction (IBC) detectors offer many significant advantages over other conventional photon detectors utilized for the infrared. SiAs offer excellent spectral response out to 28 μm with dark current in the 0.01e/second range at 7K over a wide bias range with no tunneling limitations. In addition, because of the perfect thermal match between the Si:As IBC detector and the readout IC (ROIC), hybrids formed by mating Si:As IBCs and ROICs are mechanically stable and have no hybrid reliability problems. Since Si:As IBC detectore are fabricated on readily available Si substrates, large formats are realizable. Si:As IBC detectors have been under development since the mid 80s at Raytheon Vision Systems (RVS). Under the NSAS SIRTF program, a 256 x 256 Si:As array was developed and successfully integrated into the SIRTF IRAC instrument. This same array is also utilized in the ASTRO-F IRC instrument. Both missions will be launched shortly and provide a significant improvement in our ability to measure the spectral signatures of solar type stars and galaxies at high redshifts under very low background conditions in space. Under the NASA Origins program, in collaboration with NASA Ames Research Center (ARC), RVS developed a high performance 1024 x 1024 Si:As IBC array. This array was tested at Ames Research Center. This paper will review the progress of Si:As IBC development at RVS, present test data from ARC, and discuss the more recent developments in Si:As IBC detectors for the JWST MIRI instrument and future missions such as SPICA, TPF, FIRST and DARWIN.


Proceedings of SPIE | 1993

Low-noise, low-temperature 256 x 256 Si:As IBC staring FPA

Nancy A. Lum; James F. Asbrock; Rebekah White; Raymond E. Kelchner; Larry Lum; Le T. Pham; Craig R. McCreight; Mark E. McKelvey; Robert E. McMurray; William J. Forrest; James D. Garnett

Cryogenic space telescopes such as the Space Infrared Telescope Facility (SIRTF) require large-area focal plane arrays (FPAs) with high sensitivity. Such applications set requirements for the readout arrays to simultaneously provide low noise and low power dissipation at very low temperatures. The Hughes Technology Center (HTC) has developed a low-noise 256 X 256-pixel hybrid FPA composed of a PMOS readout array hybridized to an arsenic- doped silicon (Si:As) impurity-band conduction (IBC) detector which is designed to operate below 10 K. The readout unit cell employs a switched source-follower-per-detector (SFD) design where in signals are multiplexed onto four outputs. The detector was processed using high-purity, multilayered epitaxial processing. The readout was processed using the p-channel subset of HTCs CryoCMOS process.


Astronomical Telescopes and Instrumentation | 1998

Si:As IBC IR focal plane arrays for ground-based and space-based astronomy

Arnold D. Estrada; George Domingo; James D. Garnett; Alan W. Hoffman; Nancy A. Lum; Peter J. Love; Steven Lawrence Solomon; John E. Venzon; George R. Chapman; K. P. Sparkman; Craig R. McCreight; Mark E. McKelvey; Robert E. McMurray; John A. Estrada; S. Zins; R. McHugh; Roy R. Johnson

Raytheon/SBRC has demonstrated high quality Si:As IBC IR FPAs for both ground-based and space-based Mid-IR astronomy applications. These arrays offer in-band quantum efficiencies of approximately 50 percent over a wavelength range from 6 micrometers to 26 micrometers and usable responses from 2 micrometers to 28 micrometers . For high background, ground-based applications the readout input circuit is a direct injection (DI) FET, while for low background, space-based applications a source follower per detector (SFD) is used. The SFD offers extremely low noise and power dissipation, and is implemented in a very small unit cell. The DI input circuit offers much larger bucket capacity and better linearity compared with the SFD, and is implemented in a 50 micrometers unit cell. SBRCs Si:As IBC detector process results in very low dark current sand our Raytheon/MED readout process is optimized for very low redout noise at low temperature operation. SBRC is committed to achieving still better performance to serve the future needs of the IR astronomy community.

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Daniel Y. Gezari

Goddard Space Flight Center

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Gerald M. Lamb

Goddard Space Flight Center

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Peter K. Shu

Goddard Space Flight Center

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