Technique applied in electrical power distribution for Satellite Launch Vehicle
Autor(a) principal: | |
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Data de Publicação: | 2010 |
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=S2175-91462010000300263 |
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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Journal of Aerospace Technology and Management (Online) |
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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 |
_version_ |
1754732530420940800 |