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Engineering Voyager 2's encounter with UranusChanges made by radio control from the ground in the Voyager 2 spacecraft as it approached Uranus are described. Reduced power required that subsystems and heaters had to be switched on and off in carefully synchronized fashion. Low light levels required increased exposure times, so the jiggling of the spacecraft had to be minimized. Coding changes were made and image data were compressed to cope with the reduced bit rate at larger distances. Successful efforts to cope with failures in the primary radio receiver and in the computer instructions for image compression are described, as are changes made on the ground in the spacecraft navigation.
Document ID
19870033221
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Laeser, Richard P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mclaughlin, William I.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wolff, Donna M.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
November 1, 1986
Publication Information
Publication: Scientific American
Volume: 255
ISSN: 0036-8733
Subject Category
Astronautics (General)
Report/Patent Number
ISSN: 0036-8733
Accession Number
87A20495
Distribution Limits
Public
Copyright
Other

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