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A launch vehicle stability analysis using the parameter plane methodLaunch vehicle attitude control system for lateral drift minimization and prevention of structural load limit exceeding maneuvers, presenting stability analysis
Document ID
19710036641
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Seltzer, S. M.
Date Acquired
August 6, 2013
Publication Date
October 1, 1970
Subject Category
Space Vehicles
Accession Number
71A17338
Distribution Limits
Public
Copyright
Other

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