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Optimization of step rockets by the discrete maximum principle.Optimum stage weight distribution in multistage rocket obtained by discrete maximum principle
Document ID
19660034737
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Fan, L.-T.
Hwang, C.-L.
Wang, C.-S.
Date Acquired
August 3, 2013
Publication Date
November 1, 1965
Subject Category
Space Vehicles
Report/Patent Number
ASME PAPER 64-WA/AV-5
Report Number: ASME PAPER 64-WA/AV-5
Accession Number
66A14027
Funding Number(s)
CONTRACT_GRANT: NSG-692
Distribution Limits
Public
Copyright
Other
Keywords
WEIGHT FACTOR
MULTISTAGE ROCKET
MAXIMUM PRINCIPLE

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