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Global auroral imaging instrumentation for the Dynamics Explorer MissionThe instrumentation for obtaining global images of the auroral oval from the high-altitude spacecraft of the Dynamics Explorer Mission is described. It is noted that the three spin-scan auroral imaging photometers are expected to be able to effectively view the dim emissions from earth in the presence of strong stray light sources near their fields-of-view along the sunlit portion of the spacecraft orbit. A special optical design that includes an off-axis parabolic mirror as the focusing element and super-reflecting mirror surfaces is used to minimize the effects of stray light. The rotation of the spacecraft and an instrument scanning mirror provide the two-dimensional array of pixels making up an image frame. It is pointed out that the full width of the fields-of-view of the photometers corresponding to a single pixel is 0.29 deg and that the angular dimensions of a typical full frame are 30 deg x 30 deg and span 14,400 pixels.
Document ID
19820032899
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Frank, L. A.
(Iowa Univ. Iowa City, IA, United States)
Craven, J. D.
(Iowa Univ. Iowa City, IA, United States)
Ackerson, K. L.
(Iowa Univ. Iowa City, IA, United States)
English, M. R.
(Iowa, University Iowa City, IA, United States)
Eather, R. H.
(Iowa Univ. Iowa City, IA, United States)
Carovillano, R. L.
(Iowa, University Iowa City, IA; Boston College, Chestnut Hill, MA, United States)
Date Acquired
August 10, 2013
Publication Date
December 1, 1981
Publication Information
Publication: Space Science Instrumentation
Volume: 5
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AD-A120637
Accession Number
82A16434
Funding Number(s)
CONTRACT_GRANT: NAS5-24293
CONTRACT_GRANT: NGL-16-001-002
CONTRACT_GRANT: N00014-76-C-0016
Distribution Limits
Public
Copyright
Other

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