Technique applied in electrical power distribution for Satellite Launch Vehicle

Detalhes bibliográficos
Autor(a) principal: Bizarria,Francisco Carlos P.
Data de Publicação: 2010
Outros Autores: Bizarria,José Walter Parquet, Spina,Fábio Duarte, Rosário,João Maurício
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=S2175-91462010000300263
Resumo: Abstract: The Satellite Launch Vehicle electrical network, which is currently being developed in Brazil, is sub-divided for analysis in the following parts: Service Electrical Network, Controlling Electrical Network, Safety Electrical Network and Telemetry Electrical Network. During the pre-launching and launching phases, these electrical networks are associated electrically and mechanically to the structure of the vehicle. In order to succeed in the integration of these electrical networks it is necessary to employ techniques of electrical power distribution, which are proper to Launch Vehicle systems. This work presents the most important techniques to be considered in the characterization of the electrical power supply applied to Launch Vehicle systems. Such techniques are primarily designed to allow the electrical networks, when submitted to the single-phase fault to ground, to be able of keeping the power supply to the loads.
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spelling Technique applied in electrical power distribution for Satellite Launch VehicleSLVElectrical networkPower distributionAbstract: The Satellite Launch Vehicle electrical network, which is currently being developed in Brazil, is sub-divided for analysis in the following parts: Service Electrical Network, Controlling Electrical Network, Safety Electrical Network and Telemetry Electrical Network. During the pre-launching and launching phases, these electrical networks are associated electrically and mechanically to the structure of the vehicle. In order to succeed in the integration of these electrical networks it is necessary to employ techniques of electrical power distribution, which are proper to Launch Vehicle systems. This work presents the most important techniques to be considered in the characterization of the electrical power supply applied to Launch Vehicle systems. Such techniques are primarily designed to allow the electrical networks, when submitted to the single-phase fault to ground, to be able of keeping the power supply to the loads.Departamento de Ciência e Tecnologia Aeroespacial2010-12-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462010000300263Journal of Aerospace Technology and Management v.2 n.3 2010reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.2010.02038410info:eu-repo/semantics/openAccessBizarria,Francisco Carlos P.Bizarria,José Walter ParquetSpina,Fábio DuarteRosário,João Maurícioeng2017-05-22T00:00:00Zoai:scielo:S2175-91462010000300263Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-22T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Technique applied in electrical power distribution for Satellite Launch Vehicle
title Technique applied in electrical power distribution for Satellite Launch Vehicle
spellingShingle Technique applied in electrical power distribution for Satellite Launch Vehicle
Bizarria,Francisco Carlos P.
SLV
Electrical network
Power distribution
title_short Technique applied in electrical power distribution for Satellite Launch Vehicle
title_full Technique applied in electrical power distribution for Satellite Launch Vehicle
title_fullStr Technique applied in electrical power distribution for Satellite Launch Vehicle
title_full_unstemmed Technique applied in electrical power distribution for Satellite Launch Vehicle
title_sort Technique applied in electrical power distribution for Satellite Launch Vehicle
author Bizarria,Francisco Carlos P.
author_facet Bizarria,Francisco Carlos P.
Bizarria,José Walter Parquet
Spina,Fábio Duarte
Rosário,João Maurício
author_role author
author2 Bizarria,José Walter Parquet
Spina,Fábio Duarte
Rosário,João Maurício
author2_role author
author
author
dc.contributor.author.fl_str_mv Bizarria,Francisco Carlos P.
Bizarria,José Walter Parquet
Spina,Fábio Duarte
Rosário,João Maurício
dc.subject.por.fl_str_mv SLV
Electrical network
Power distribution
topic SLV
Electrical network
Power distribution
description Abstract: The Satellite Launch Vehicle electrical network, which is currently being developed in Brazil, is sub-divided for analysis in the following parts: Service Electrical Network, Controlling Electrical Network, Safety Electrical Network and Telemetry Electrical Network. During the pre-launching and launching phases, these electrical networks are associated electrically and mechanically to the structure of the vehicle. In order to succeed in the integration of these electrical networks it is necessary to employ techniques of electrical power distribution, which are proper to Launch Vehicle systems. This work presents the most important techniques to be considered in the characterization of the electrical power supply applied to Launch Vehicle systems. Such techniques are primarily designed to allow the electrical networks, when submitted to the single-phase fault to ground, to be able of keeping the power supply to the loads.
publishDate 2010
dc.date.none.fl_str_mv 2010-12-01
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=S2175-91462010000300263
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462010000300263
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.2010.02038410
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.2 n.3 2010
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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