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  • 1
    Publication Date: 2006-02-14
    Description: The initial testing performed on the Hughes Metal Oxide Semiconductor Direct Readout (MOS DRO) with a Si:In extrinsic infrared array is described. The testing to date was of a screening nature and the results are primarily qualitative rather than quantitative. At a later date the performance optimization phase will be initiated. An encouraging result is that this response is strongly dependent on the detector temperature, to the extent that thermal transients introduced during the chip readout will affect the performance. A responsivity of 1 A/W at 2.2 microns with a bias of 15 volts, which is well below what is optimum bias, was obtained.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA. Ames Research Center Proceedings of the Second Infrared Detector Technology Workshop; 12 p
    Format: text
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  • 2
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    In:  Other Sources
    Publication Date: 2011-08-16
    Description: A method for measurement of temperature in the earth's lower thermosphere from a high-velocity probes is described. An undisturbed atmospheric sample is admitted to the instrument by means of a free molecular flow inlet system of skimmers which avoids surface collisions of the molecules prior to detection. Measurement of the time-of-flight distribution of an initially well-localized group of nitrogen metastable molecular states produced in an open, crossed electron-molecular beam source, yields information on the atmospheric temperature. It is shown that for high vehicle velocities, the time-of-flight distribution of the metastable flux is a sensitive indicator of atmospheric temperature. The temperature measurement precision should be greater than 94% at the 99% confidence level over the range of altitudes from 120-170 km. These precision and altitude range estimates are based on the statistical consideration of the counting rates achieved with a multichannel analyzer using realistic values for system parameters.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Format: text
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  • 3
    Publication Date: 2011-08-19
    Description: An algorithm is presented for the construction of images using linear array data with nonuniform scan coverage of object space and nonuniform detector responses. The algorithm achieves the maximum correlation between adjacent pixels, i.e., the smoothest image, consistent with the data and data uncertainties. For high spatial data density and signal-to-noise ratio, the achievable spatial resolution can exceed the diffraction limit of the optics. The capability of the algorithm is illustrated using 60-micron data from the region centered on the galaxy M101, obtained during the all-sky survey performed by the Infrared Astronomical Satellite. The 60-micron map produced has a resolution of about 36 arcsec and allows the identification of many H II regions by position and aperture photometry for the brighter ones. The achieved resolution is discussed in terms of the a priori estimate of the mean correlation length of the data, the directly measured FWHM in the final image, and the results of aperture photometry of M101 H II regions NGC 5447, 5455, 5461, 5462 and 5471.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: Astronomical Journal (ISSN 0004-6256); 99; 1674-168
    Format: text
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  • 4
    Publication Date: 2019-05-29
    Description: Accurate wide range ultrahigh vacuum gauge calibration method using pressure attenuation, atomic beam, and cryopumping techniques to evaluate system components and performance
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-CR-75529
    Format: application/pdf
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  • 5
    Publication Date: 2019-06-27
    Description: The OGO-4 main body airglow photometer used a trialkali cathode photomultiplier to sense light at selected wavelengths between 2500 and 6300A corresponding to important emissions in the aurora and night airglow at emission rates ranging from a few rayleighs to about 200 kilorayleighs. The optical, electronic, and mechanical systems are described in terms of their functional characteristics.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-TM-X-65926 , X-625-72-174 , NSSDC-ID-65-081A-10-PM , NSSDC-ID-67-073A-12-PM
    Format: application/pdf
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  • 6
    Publication Date: 2019-06-27
    Description: The sampling probe to measure the free stream gas composition in a hypersonic wind tunnel is described. Using a free expansion of the continuum flow, a series of sampling inlet-pumping stages is evaluated. Mass analysis is carried out with a quadrupole mass spectrometer employing a crossed electron beam, molecular beam ion source, and an off-axis electron multiplier. The spatial distribution of the sampled molecular flux and the pumping requirements are evaluated for varying inlet conditions of gas density and flow velocity. The signal-to-noise ratio of the molecular beam formed by this series of coaxial inlets is also determined. The signal-to-noise ratio of the unscattered flux is sufficiently high that an unambiguous determination of the beam composition and of the free stream gas properties can be made. The magnitude of the detected signal is sufficiently high that measurement of trace constituents two orders of magnitude below the primary beam signal can be made.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-CR-111986
    Format: application/pdf
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  • 7
    Publication Date: 2019-06-27
    Description: Diffusers for in-flight calibration of detectors installed in spacecraft
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-CR-987
    Format: application/pdf
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  • 8
    Publication Date: 2019-06-27
    Description: Calibration method and ultrahigh vacuum components for ionization gage and mass spectrometer
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-CR-100367
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  • 9
    Publication Date: 2019-06-27
    Description: Design and construction of mass spectrometer using cold cathode source of ions, quadrupole mass analyzer, and ion counting detectors
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-CR-1475
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  • 10
    Publication Date: 2019-06-27
    Description: Fabrication and testing of the magnetic control assembly (MCA) are summarized. The MCA was designed as an add-on unit for certain existing components of the Nimbus and ERTS attitude control system. The MCA system consists of three orthogonal electromagnets; a magnetometer probe capable of sensing external fields in the X, Y, and Z axes; and the control electronics. An operational description of the system is given along with all major drawings and photographs. Manufacturing and inspection procedures are outlined and a chronological list of events is included with the fabrication summary.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-CR-130142 , REPT-90569
    Format: application/pdf
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