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contributor authorLiang-Tseng Fan
contributor authorChing-Lai Hwang
contributor authorChiu-Sen Wang
date accessioned2017-05-08T23:35:29Z
date available2017-05-08T23:35:29Z
date copyrightNovember, 1965
date issued1965
identifier issn1087-1357
identifier otherJMSEFK-27495#419_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108523
description abstractThe general algorithm of the discrete maximum principle with information feedback is stated briefly. It is applied to obtain solutions for the optimum stage-weight distribution problems of a multistage rocket vehicle. The first problem treats the structure ratio as a constant in each stage, though it may differ stage by stage. The second problem considers the variations in structural factors with stage weight. The third problem obtains the optimum weight distribution which minimizes hardware weight. Specific examples are solved.
publisherThe American Society of Mechanical Engineers (ASME)
titleOptimization of Step Rockets by the Discrete Maximum Principle
typeJournal Paper
journal volume87
journal issue4
journal titleJournal of Manufacturing Science and Engineering
identifier doi10.1115/1.3670855
journal fristpage419
journal lastpage424
identifier eissn1528-8935
keywordsOptimization
keywordsRockets
keywordsWeight (Mass)
keywordsHardware
keywordsAlgorithms
keywordsVehicles AND Feedback
treeJournal of Manufacturing Science and Engineering:;1965:;volume( 087 ):;issue: 004
contenttypeFulltext


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