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Postflight evaluation of the solar maximum spacecraft magnetometersThe Solar Maximum Mission spacecraft was launched February 14, 1980 from Cape Kennedy. Attached to one side of the spacecraft was the Modular Attitude Control System (MACS). Two Schonstedt magnetometers were located within the MACS module. Although primarily used as a backup attitude determination system during the Solar Maximum Repair Mission, the magnetometers were instrumental in stabilizing the spacecraft. In October of 1984 the Solar Maximum magnetometers were returned to Schonstedt Instrument Company for postflight analysis, where they were subjected to the same electrical performance tests performed prior to use. In both instances the magnetometer performance was exceptional. Postflight test data nearly duplicated preflight test data.
Document ID
19870004947
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dunham, W. D.
(Schonstedt Instrument Co. Reston, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA. Goddard Space Flight Center Proceedings of the SMRM Degradation Study Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N14380
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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