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Charge injection device as a candidate sensor for stellar trackingCharge transfer devices (CTDs) are superior to the image dissector as stellar tracking sensors, considering their low voltage requirements, insensitivity to magnetic fields, good linearity, and low weight and power. An analysis of one type of CTD, called the charge injection device (CID), revealed an X-Y addressing capability which provides exceptional flexibility in array readout and results in enhanced S/N capability, a surface channel device which produces a larger dynamic range of operation, and exceptional and unique tolerance to optical overloads. A 128 row by 128 column CID array processed on silicon was evaluated in a cooled breadboard camera, and measured results indicate projected performance parameters of a large area CID array as follows: 20 micron square sensing site, noise not greater than 25 carriers per pixel, quantum yield of approximately 40% from 0.4 to 1.0 micron, and cooling requirements on the order of 0 degrees C.
Document ID
19800033282
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Jones, C. S., Jr.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Michon, G. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Burke, H. K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Vogelsong, T. L.
(General Electric Co. Schenectady, N.Y., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Instrumentation
Meeting Information
Meeting: Space optics
Location: Huntsville, AL
Start Date: May 22, 1979
End Date: May 24, 1979
Accession Number
80A17452
Distribution Limits
Public
Copyright
Other

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