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Rocket trajectory optimization by a second- order numerical technique.Multistage rocket trajectories optimized by second order numerical technique and digital computer program, considering coasting, vacuum flight and transition times
Document ID
19690054165
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kelley, H. J.
Mckay, S. S., II
Uzzell, B. R.
Date Acquired
August 5, 2013
Publication Date
May 1, 1969
Subject Category
Space Sciences
Accession Number
69A32154
Funding Number(s)
CONTRACT_GRANT: NAS9-4036
Distribution Limits
Public
Copyright
Other

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