Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications

Detalhes bibliográficos
Autor(a) principal: Lobanov,Leonid M.
Data de Publicação: 2016
Outros Autores: Volkov,Valentin S., Yakimkin,Alexander V., Savitsky,Viktor V.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000100055
Resumo: ABSTRACT Under conditions of the influence of space environment factors, the thin-walled load-carrying transformable-volume structures are subjected to volumetric deformation and long-time exposure to external loads, close to maximum permissible design values. The required functional properties of transformable-volume structures are ensured on the basis of applying surface engineering methods, whose effectiveness is difficult to confirm as there is no possibility to reproduce the space environment factors complex under the terrestrial conditions. The method for verification of applied technologies regarding the modification of surface properties was described. It was based on the comparison of finite-element and experimental-computational models of displacements in equivalent fragments of the transformablevolume structures surface. Qualitative and quantitative evaluation of methods is given, allowing changing the rigiditystrength characteristics of transformable-volume structures for space applications without alteration of their mass and compactness.
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spelling Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space ApplicationsTransformable-volume structuresSurface engineeringNon-destructive testingElectron shearographyLoad-carrying shellsFoldable shellsABSTRACT Under conditions of the influence of space environment factors, the thin-walled load-carrying transformable-volume structures are subjected to volumetric deformation and long-time exposure to external loads, close to maximum permissible design values. The required functional properties of transformable-volume structures are ensured on the basis of applying surface engineering methods, whose effectiveness is difficult to confirm as there is no possibility to reproduce the space environment factors complex under the terrestrial conditions. The method for verification of applied technologies regarding the modification of surface properties was described. It was based on the comparison of finite-element and experimental-computational models of displacements in equivalent fragments of the transformablevolume structures surface. Qualitative and quantitative evaluation of methods is given, allowing changing the rigiditystrength characteristics of transformable-volume structures for space applications without alteration of their mass and compactness.Departamento de Ciência e Tecnologia Aeroespacial2016-03-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000100055Journal of Aerospace Technology and Management v.8 n.1 2016reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v8i1.529info:eu-repo/semantics/openAccessLobanov,Leonid M.Volkov,Valentin S.Yakimkin,Alexander V.Savitsky,Viktor V.eng2016-07-21T00:00:00Zoai:scielo:S2175-91462016000100055Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2016-07-21T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications
title Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications
spellingShingle Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications
Lobanov,Leonid M.
Transformable-volume structures
Surface engineering
Non-destructive testing
Electron shearography
Load-carrying shells
Foldable shells
title_short Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications
title_full Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications
title_fullStr Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications
title_full_unstemmed Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications
title_sort Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications
author Lobanov,Leonid M.
author_facet Lobanov,Leonid M.
Volkov,Valentin S.
Yakimkin,Alexander V.
Savitsky,Viktor V.
author_role author
author2 Volkov,Valentin S.
Yakimkin,Alexander V.
Savitsky,Viktor V.
author2_role author
author
author
dc.contributor.author.fl_str_mv Lobanov,Leonid M.
Volkov,Valentin S.
Yakimkin,Alexander V.
Savitsky,Viktor V.
dc.subject.por.fl_str_mv Transformable-volume structures
Surface engineering
Non-destructive testing
Electron shearography
Load-carrying shells
Foldable shells
topic Transformable-volume structures
Surface engineering
Non-destructive testing
Electron shearography
Load-carrying shells
Foldable shells
description ABSTRACT Under conditions of the influence of space environment factors, the thin-walled load-carrying transformable-volume structures are subjected to volumetric deformation and long-time exposure to external loads, close to maximum permissible design values. The required functional properties of transformable-volume structures are ensured on the basis of applying surface engineering methods, whose effectiveness is difficult to confirm as there is no possibility to reproduce the space environment factors complex under the terrestrial conditions. The method for verification of applied technologies regarding the modification of surface properties was described. It was based on the comparison of finite-element and experimental-computational models of displacements in equivalent fragments of the transformablevolume structures surface. Qualitative and quantitative evaluation of methods is given, allowing changing the rigiditystrength characteristics of transformable-volume structures for space applications without alteration of their mass and compactness.
publishDate 2016
dc.date.none.fl_str_mv 2016-03-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000100055
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000100055
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v8i1.529
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.8 n.1 2016
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
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