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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
19650030705
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fan, L.-T.
Hwang, C.-L.
Wang, C.-S.
Date Acquired
August 2, 2013
Publication Date
November 1, 1964
Subject Category
Space Vehicles
Report/Patent Number
ASME PAPER 64-WA/AV-5
Report Number: ASME PAPER 64-WA/AV-5
Accession Number
65A13409
Funding Number(s)
CONTRACT_GRANT: NSG-692
Distribution Limits
Public
Copyright
Other
Keywords
MULTISTAGE ROCKET
MAXIMUM PRINCIPLE
WEIGHT FACTOR

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