Functional Characteristics Improvement of Metal Transformable-Volume Structures for Space Applications
Autor(a) principal: | |
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Data de Publicação: | 2016 |
Outros Autores: | , , |
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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Journal of Aerospace Technology and Management (Online) |
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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 |
_version_ |
1754732531284967424 |