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contributor authorIrvin Krause
contributor authorBernard W. Shaffer
date accessioned2017-05-08T23:06:36Z
date available2017-05-08T23:06:36Z
date copyrightFebruary, 1962
date issued1962
identifier issn1087-1357
identifier otherJMSEFK-27458#144_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92068
description abstractExpressions are derived for the bond stresses induced by a radially symmetric temperature distribution in spherical propellant grains bonded to spherical casings. Equations for the evaluation of radial and tangential stresses in the propellant and its casing have also been derived. Both solid and hollow propellant grains have been investigated. Design considerations have been developed to enable the designer to minimize the bond stress. A comparison between the hollow and solid spherical propellant assembly shows that the hollow sphere has a lower bond stress than the solid sphere, assuming all other factors are the same.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermal Stresses in Spherical Case-Bonded Propellant Grains
typeJournal Paper
journal volume84
journal issue1
journal titleJournal of Manufacturing Science and Engineering
identifier doi10.1115/1.3667394
journal fristpage144
journal lastpage148
identifier eissn1528-8935
keywordsThermal stresses
keywordsPropellants
keywordsStress
keywordsManufacturing
keywordsDesign
keywordsEquations AND Temperature distribution
treeJournal of Manufacturing Science and Engineering:;1962:;volume( 084 ):;issue: 001
contenttypeFulltext


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