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Absolute stability analysis of attitude control systems for large boostersAbsolute stability analysis of attitude control systems for large launch vehicles
Document ID
19710017455
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Seltzer, S. M. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Siljak, D. D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
April 2, 1971
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-64582
Report Number: NASA-TM-X-64582
Accession Number
71N26931
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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