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The OSO-7 missionAddition of a gyro and star sensor to the wheel section of OSO-G provided nighttime pointing capability and functional redundancy in correcting an anomaly that put the combined OSO spacecraft and launch vehicle into a flat spin.
Document ID
19730019085
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Thole, J. M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Publication Information
Publication: Significant Accomplishments in Technol., 1972
Subject Category
Space Vehicles
Accession Number
73N27817
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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