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Boundary-layer approximation to powered-flight attitude transientsRocket vehicle flight optimization for model including rigid body degrees of freedom in boundary layer approximation to attitude transients
Document ID
19700059548
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kelley, H. J.
Date Acquired
August 5, 2013
Publication Date
July 1, 1970
Subject Category
Space Vehicles
Accession Number
70A35664
Funding Number(s)
CONTRACT_GRANT: NAS5-11738
Distribution Limits
Public
Copyright
Other

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