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Dive into the research topics where Robert J. Martineau is active.

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Featured researches published by Robert J. Martineau.


SPIE's 1996 International Symposium on Optical Science, Engineering, and Instrumentation | 1996

Cassini infrared Fourier spectroscopic investigation

Virgil G. Kunde; Peter A. R. Ade; Richard D. Barney; D. Bergman; Jean-Francois Bonnal; R. Borelli; David Boyd; John C. Brasunas; Gregory Vallee Brown; Simon B. Calcutt; F. Carroll; R. Courtin; Jacky B. Cretolle; Julie A. Crooke; Martin A. Davis; S. Edberg; Rainer K. Fettig; M. Flasar; David A. Glenar; S. Graham; John G. Hagopian; Claef Hakun; Patricia Ann Hayes; L. Herath; Linda J. Spilker; Donald E. Jennings; Gabriel Karpati; C. Kellebenz; Brook Lakew; J. Lindsay

The composite infrared spectrometer (CIRS) is a remote sensing instrument to be flown on the Cassini orbiter. CIRS will retrieve vertical profiles of temperature and gas composition for the atmospheres of Titan and Saturn, from deep in their tropospheres to high in their stratospheres. CIRS will also retrieve information on the thermal properties and composition of Saturns rings and Saturnian satellites. CIRS consists of a pair of Fourier Transform Spectrometers (FTSs) which together cover the spectral range from 10-1400 cm-1 with a spectral resolution up to 0.5 cm-1. The two interferometers share a 50 cm beryllium Cassegrain telescope. The far-infrared FTS is a polarizing interferometer covering the 10-600 cm-1 range with a pair of thermopile detectors, and a 3.9 mrad field of view. The mid-infrared FTS is a conventional Michelson interferometer covering 200-1400 cm-1 in two spectral bandpasses: 600-1100 cm- 1100-1400 cm(superscript -1 with a 1 by 10 photovoltaic HgCdTe array. Each pixel of the arrays has an approximate 0.3 mrad field of view. The HgCdTe arrays are cooled to approximately 80K with a passive radiative cooler.


Publications of the Astronomical Society of the Pacific | 2007

Detectors for the James Webb Space Telescope Near‐Infrared Spectrograph. I. Readout Mode, Noise Model, and Calibration Considerations

Bernard J. Rauscher; Ori D. Fox; Pierre Ferruit; Robert J. Hill; Augustyn Waczynski; Yiting Wen; Wei Xia-Serafino; Brent Mott; D. M. Alexander; Clifford K. Brambora; Rebecca Derro; Chuck Engler; Matthew B. Garrison; Tom Johnson; Sridhar S. Manthripragada; James M. Marsh; Cheryl J. Marshall; Robert J. Martineau; Kamdin B. Shakoorzadeh; Donna Wilson; Wayne D. Roher; Miles Smith; Craig A. Cabelli; James D. Garnett; Markus Loose; Selmer Wong‐Anglin; Majid Zandian; Edward S. Cheng; Timothy Ellis; Bryan Howe

We describe how the James Webb Space Telescope (JWST) Near-Infrared Spectrographs (NIRSpec) detectors will be read out, and present a model of how noise scales with the number of multiple nondestructive reads sampling up the ramp. We believe that this noise model, which is validated using real and simulated test data, is applicable to most astronomical near-infrared instruments. We describe some nonideal behaviors that have been observed in engineering-grade NIRSpec detectors, and demonstrate that they are unlikely to affect NIRSpec sensitivity, operations, or calibration. These include a HAWAII-2RG reset anomaly and random telegraph noise (RTN). Using real test data, we show that the reset anomaly is (1) very nearly noiseless and (2) can be easily calibrated out. Likewise, we show that large-amplitude RTN affects only a small and fixed population of pixels. It can therefore be tracked using standard pixel operability maps.


Proceedings of SPIE | 2006

Detectors for the James Webb Space Telescope near infrared spectrograph (NIRSpec)

Bernard J. Rauscher; Torsten Böker; Craig A. Cabelli; Guido De Marchi; Pierre Ferruit; James D. Garnett; Robert J. Hill; Markus Loose; Michael W. Regan; Augustyn Waczynski; Yiting Wen; Selmer Wong; M. Zandian; David Alexander; Clifford K. Brambora; Rebecca Derro; Carol Dunn; Tim Ellis; Matthew B. Garrison; Bryan Howe; P. J. Jakobsen; Thomas E. Johnson; Miriam Jurado; Ginn Lee; Sridhar S. Manthripragada; James M. Marsh; Cheryl J. Marshall; Robert J. Martineau; Brent Mott; John Nieznanski

The Near Infrared Spectrograph (NIRSpec) will be the James Webb Space Telescopes (JWSTs) primary near-infrared spectrograph. NIRSpec is a multi-object spectrograph with fixed-slit and integral field modes. EADS/Astrium is building NIRSpec for the European Space Agency (ESA), with NASA is providing the detector subsystem and programmable multi-aperture mask. In this paper, we summarize recent progress on the detector subsystem including tests demonstrating that JWSTs Rockwell HAWAII-2RG sensor chip assemblies have achieved Technology Readiness Level 6 (TRL-6). Achieving TRL-6 is an important milestone because TRL-6 is required for flight.


lasers and electro-optics society meeting | 2006

Large format HgCdTe arrays for the James Webb Space Telescope

Brent Mott; Torsten Böker; Craig A. Cabelli; G. De Marchi; P. Ferruit; James D. Garnett; Robert J. Hill; Markus Loose; Bernard J. Rauscher; Michael W. Regan; Augustyn Waczynski; Yiting Wen; Selmer Wong; M. Zandian; D. M. Alexander; Clifford K. Brambora; Rebecca Derro; C. Dunn; Tim Ellis; Matthew B. Garrison; Bryan Howe; P. J. Jakobsen; Thomas E. Johnson; Miriam Jurado; Ginn Lee; Sridhar S. Manthripragada; James M. Marsh; Cheryl J. Marshall; Robert J. Martineau; John Nieznanski

The near infrared spectrograph (NIRSpec) will be the James Webb Space Telescopes (JWSTs) primary near-infrared spectrograph. NIRSpec is a multi-object spectrograph with fixed-slit and integral field modes. EADS/Astrium is building NIRSpec for the European Space Agency (ESA), with NASA providing the detector subsystem and programmable multi-aperture mask. In this presentation we present an overview of the detector subsystem (DS)


Astronomical Telescopes and Instrumentation | 2000

Detector requirements for NGST

Craig R. McCreight; Albert M. Fowler; Thomas P. Greene; Matthew A. Greenhouse; Donald N. B. Hall; Knox S. Long; John W. MacKenty; Robert J. Martineau; Judith L. Pipher; Michael E. Ressler; Erick T. Young

This paper summarizes the findings of the Next Generation Space Telescope (NGST) Detector Requirements Review Panel. This panel was comprised of NGST Integrated Science Instrument Module study representatives, detector specialists, and members of the NGST project science team. It has produced a report that recommends detector performance levels, and has provided rationale for deriving these levels from basic, anticipated NGST science goals and programs. Key parameters such as detector array format, quantum efficiency, and noise are discussed and prioritized.


Optical Science, Engineering and Instrumentation '97 | 1997

PC detector passivation for high performance

Robert J. Martineau; Zhiqing Shi; Kelley Hu; Sridhar S. Manthripragada; F. A. Peters; Andre S. Burgess; John Godfrey; Danny J. Krebs

Probably the most important factor in producing HgCdTe detectors of high performance is surface passivation. A good passivant for PC HgCdTe detectors accumulates the surface thereby reflecting minority carriers from surface imperfections and increasing minority carrier lifetime. A variety of passivants are known and used to various degrees, including sulfides, fluorides, oxides, and others. One of the problems with known passivants is that they tend to accumulate the surface too strongly, thus producing non-optimal results. We have developed a new passivation process which passivates the surface without strong accumulation. This results in detector resistance that is about 50%higher than that achieved with traditional KOH passivation, responsivities that are from 100 to 200% higher, and detectivities that are from 50to 100% higher for long wavelength devices. Materials and processing details used to achieve these results, as well as experimental data will be presented. Keyword: passivation, infrared, HgCdTe, detector


SPIE's 1996 International Symposium on Optical Science, Engineering, and Instrumentation | 1996

HgCdTe detector technology and performance for the Composite Infrared Spectrometer (CIRS)/Cassini mission

Robert J. Martineau; Kelley Hu; Sridhar S. Manthripragada; Carl A. Kotecki; R. Sachidananda Babu; F. A. Peters; Andre S. Burgess; David Brent Mott; Danny J. Krebs; S. Graham; Audrey J. Ewin; Avery I. Miles; Vincent T. Bly; Trang L. Nguyen; J. McCloskey; Peter K. Shu

The composite infrared spectrometer (CIRS) instrument, an important component of the Cassini mission, consists of 3 focal plane arrays for sensing IR radiation of the Saturnian planetary system. Goddard Space Flight Center has fabricated, tested, and delivered high performance, 10- element HgCdTe photoconductive (PC) arrays for use on CIRS FP3, the focal plane responsible for detection of radiation in the 9.1 to 16.7 micrometers spectral band. The delivered flight array has peak responsivity 100 percent above CIRS specification, detectivity 30 percent or more above specification, and a cutoff wavelength of 17.3 micrometers at the operating temperature of 80 K. In order to achieve high performance at low frequency while maintaining limited power dissipation, we adopted a split-geometry detector structure. This design also ensured the buttability of the PC arrays to photovoltaic arrays supplied by CE-Saclay-France for detection of radiation in the 7.1 to 9.1 micrometers range. The detector structure is also noteworthy for its use of 0.05 micrometers Alumina powder-loaded epoxy to minimize reflection at the epoxy/HgCdTe interface, thus spoiling undesired optical resonance. This was done in order to meet the CIRS spectral uniformity requirement, which would have been difficult at these long wavelengths without this feature.


SPIE's 1996 International Symposium on Optical Science, Engineering, and Instrumentation | 1996

High-performance HgCdTe infrared detectors for the GOES long-wave sounder

Robert J. Martineau; Kelley Hu; Sridhar S. Manthripragada; Zhiqing Shi; Carl A. Kotecki; F. A. Peters; Andre S. Burgess; Danny J. Krebs; Roy R. Johnson; David Brent Mott; Peter K. Shu

GOES long wave sounder (LWS) detector requirements have always pushed the state-of-the-art for longwave detectors operating in the vicinity of 102 K. Performance and yield of acceptable detectors have always been problems and continue to be important issues affecting the performance of instruments of both present and future design. GSFC has been examining new device and operational concepts aimed at producing significant improvements in performance and yield. Our approach has been directed towards mitigating the deleterious effects of operating small geometry HgCdTe PC devices under heavy bias, that is, under minority carrier sweepout, as is typical in conventional LWS detector operation. Specifically, theory indicates that detectors of the new design operating under optimal bias conditions have significantly higher responsivity, lower power dissipation,and lower 1/f noise knees than conventional LWS detectors. In this paper we will describe the new LWS detectors fabricated at GSFC, present detector data, and review the theory of operation of these devices.


Space technology and applications international forum - 1998 | 2008

Split-geometry detectors, our eyes in space

Robert J. Martineau; F. A. Peters; Andre S. Burgess; Carl A. Kotecki; Sridhar S. Manthripragada; J. Godfrey; Danny J. Krebs; David Brent Mott; Peter K. Shu; J. Z. Shi; Kelley Hu

Infrared detectors have projected our ability to explore our planet and our solar system far beyond the spatial, temporal, and spectral limitations of our natural vision. As such, they are our eyes in space, constantly searching the heavens, and sending back information about the origin, constitution, and dynamics of planetary atmospheres, and other processes of interest. Their ability to do this effectively depends on their sensitivity. Today, long wave PC (photoconductive) HgCdTe detectors are the detectors of choice for applications requiring high sensitivity at long wavelengths and elevated temperature. However, planetary exploration and space surveillance of the earth’s climatic condition are presently still limited by the sensitivity of available detectors. This paper will describe detectors developed at Goddard to provide enhanced performance for applications such as the CIRS/Cassini mission to Saturn and Titan, and the GOES weather satellite. Specifically, this paper will show theoretically and experimentally how detectors of split-geometry design can be exploited to increase detector resistance, responsivity, and detectivity, while decreasing 1/f noise and power dissipation. Photomicrographs of split-geometry detectors will be shown, and data demonstrating theoretical split-geometry design advantages will be presented for flight arrays built for the CIRS/Cassini mission, and for advanced detectors for GOES.


SPIE's International Symposium on Optical Science, Engineering, and Instrumentation | 1999

Advanced Geosynchronous Studies Imager: focal plane design

Randy Kindsfather; Ronald Kraus; Robert J. Martineau

A focal plane system to generate images in 18 spectral channels ranging from visible to long-wave IR has been designed for the AGSI. The system is a line scan imager, comprised for four focal planes populated with linear detector arrays optimized for operating in the various AGSI spectral regions. Light from the AGSI telescope is diverted to the focal planes by spectrally tuned dichroic beam splitters. At the focal planes narrowband interference filters placed in close proximity to the detector arrays further filter the light. Multispectral silicon CCDs are used for visible and near IR channels. Key to system performance is the ability to use time delay and integration (TDI) in some of the narrower or less photon rich spectral channels. Detector arrays are supported by highly modular and therefore flexible and low risk signal processing and control circuits. Performance predictions have been generated for all of the spectral channels and show that the focal planes will meet or exceed NASAs requirements for an advanced imaging observatory to observe weather and climate processes and NOAAs requirements for an advanced GOES imager.

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Andre S. Burgess

Goddard Space Flight Center

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Danny J. Krebs

Goddard Space Flight Center

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F. A. Peters

Goddard Space Flight Center

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Carl A. Kotecki

Goddard Space Flight Center

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David Brent Mott

Goddard Space Flight Center

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Peter K. Shu

Goddard Space Flight Center

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Augustyn Waczynski

Goddard Space Flight Center

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