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Inversion of spin-stabilized spacecraft by mass translation - Some practical aspectsSpin stabilized spacecraft inversion by mass translation with momentum vector fixed in inertial space, calculating control mass dynamics
Document ID
19710062080
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Beachley, N. H.
Date Acquired
August 6, 2013
Publication Date
October 1, 1971
Subject Category
Space Vehicles
Accession Number
71A42777
Distribution Limits
Public
Copyright
Other

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