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Infrared spectrometer for VoyagerThe Voyager IR investigation is described, which uses a Michelson interferometer in the 180-2500/cm range, and a single-channel radiometer for the visible and near-IR, sharing a 50-cm diameter telescope. Emphasis is placed on the differences between the Voyager and the previous designs, including reductions in the field of view and in the noise equivalent spectral radiance of the instrument. Attention is given to the optical layout, the electronics module, power supply placement, thermal control heaters and flash heaters, data reduction, and calibration. A sample spectrum of Jupiter is also discussed.
Document ID
19800049628
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hanel, R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Crosby, D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Herath, L.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Vanous, D.
(Martin Marietta Aerospace Orlando, Fla., United States)
Collins, D.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Creswick, H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Harris, C.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Rhodes, M.
(Texas Instruments, Inc. Dallas, Tex., United States)
Date Acquired
August 10, 2013
Publication Date
May 1, 1980
Publication Information
Publication: Applied Optics
Volume: 19
Subject Category
Astronomy
Accession Number
80A33798
Distribution Limits
Public
Copyright
Other

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