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The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara

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Resumo:ABSTRACT: This paper introduces a new approach to represent the rocket exhaust effluents into an atmospheric dispersion model considering the trajectory and variable burning rates of a Satellite Vehicle Launcher, taking into account the buoyancy of the exhausted gases. It presents a simulation for a Satellite Vehicle Launcher flight at 12:00Z in a typical day of the dry season (Sept 17, 2008) at the Centro de Lançamento de Alcântara using the Weather Research and Forecasting Model coupled with a modified chemistry module to take into account the gases HCl, CO, CO2, and particulate matter emitted from the rocket engine. The results show that the HCl levels are dangerous in the first hour after the launching into the Launch Preparation Area and at the Technical Meteorological Center region; the CO levels are critical for the first 10 min after the launching, representing a high risk for human activities at the proximities of the launching pad.
Autores principais:Schuch,Daniel
Outros Autores:Fisch,Gilberto
Assunto:Satellite Vehicle Launcher Mesoscale model Atmospheric dispersion model HCl
Ano:2017
País:Brasil
Tipo de documento:artigo
Tipo de acesso:acesso aberto
Instituição associada:IBICT
Idioma:inglês
Origem:Oasisbr
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author Schuch,Daniel
author2 Fisch,Gilberto
author2_role author
author_facet Schuch,Daniel
Fisch,Gilberto
author_role author
country_str BR
creators_json_txt [{\"Person.name\":\"Schuch,Daniel\"},{\"Person.name\":\"Fisch,Gilberto\"}]
datacite.creators.creator.creatorName.fl_str_mv Schuch,Daniel
Fisch,Gilberto
datacite.rights.fl_str_mv http://purl.org/coar/access_right/c_abf2
datacite.subjects.subject.fl_str_mv Satellite Vehicle Launcher
Mesoscale model
Atmospheric dispersion model
HCl
datacite.titles.title.fl_str_mv The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara
dc.creator.none.fl_str_mv Schuch,Daniel
Fisch,Gilberto
dc.format.none.fl_str_mv text/html
dc.identifier.none.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462017000200137
dc.language.none.fl_str_mv eng
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.rights.none.fl_str_mv http://purl.org/coar/access_right/c_abf2
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.9 n.2 2017
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
dc.subject.none.fl_str_mv Satellite Vehicle Launcher
Mesoscale model
Atmospheric dispersion model
HCl
dc.title.fl_str_mv The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara
dc.type.none.fl_str_mv http://purl.org/coar/resource_type/c_6501
description ABSTRACT: This paper introduces a new approach to represent the rocket exhaust effluents into an atmospheric dispersion model considering the trajectory and variable burning rates of a Satellite Vehicle Launcher, taking into account the buoyancy of the exhausted gases. It presents a simulation for a Satellite Vehicle Launcher flight at 12:00Z in a typical day of the dry season (Sept 17, 2008) at the Centro de Lançamento de Alcântara using the Weather Research and Forecasting Model coupled with a modified chemistry module to take into account the gases HCl, CO, CO2, and particulate matter emitted from the rocket engine. The results show that the HCl levels are dangerous in the first hour after the launching into the Launch Preparation Area and at the Technical Meteorological Center region; the CO levels are critical for the first 10 min after the launching, representing a high risk for human activities at the proximities of the launching pad.
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organization_str_mv urn:organizationAcronym:oasisbr
person_str_mv Schuch,Daniel
Fisch,Gilberto
publishDate 2017
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
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spelling The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de AlcântaraSchuch,DanielFisch,GilbertoSatellite Vehicle LauncherMesoscale modelAtmospheric dispersion modelHClopen accesshttp://purl.org/coar/access_right/c_abf2http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462017000200137URLhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462017000200137URLHasVersion2017-06-01ABSTRACT: This paper introduces a new approach to represent the rocket exhaust effluents into an atmospheric dispersion model considering the trajectory and variable burning rates of a Satellite Vehicle Launcher, taking into account the buoyancy of the exhausted gases. It presents a simulation for a Satellite Vehicle Launcher flight at 12:00Z in a typical day of the dry season (Sept 17, 2008) at the Centro de Lançamento de Alcântara using the Weather Research and Forecasting Model coupled with a modified chemistry module to take into account the gases HCl, CO, CO2, and particulate matter emitted from the rocket engine. The results show that the HCl levels are dangerous in the first hour after the launching into the Launch Preparation Area and at the Technical Meteorological Center region; the CO levels are critical for the first 10 min after the launching, representing a high risk for human activities at the proximities of the launching pad.engtext/htmlDepartamento de Ciência e Tecnologia AeroespacialJournal of Aerospace Technology and Management v.9 n.2 2017reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTAjournal articlehttp://purl.org/coar/resource_type/c_6501literatureVoRhttp://purl.org/coar/version/c_970fb48d4fbd8a85
spellingShingle The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara
Schuch,Daniel
Satellite Vehicle Launcher
Mesoscale model
Atmospheric dispersion model
HCl
status SINGLETON
status_str VoR
subject.fl_str_mv Satellite Vehicle Launcher
Mesoscale model
Atmospheric dispersion model
HCl
title The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara
title_full The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara
title_fullStr The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara
title_full_unstemmed The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara
title_short The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara
title_sort The Use of an Atmospheric Model to Simulate the Rocket Exhaust Effluents Transport and Dispersion for the Centro de Lançamento de Alcântara
topic Satellite Vehicle Launcher
Mesoscale model
Atmospheric dispersion model
HCl
topic_facet Satellite Vehicle Launcher
Mesoscale model
Atmospheric dispersion model
HCl
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462017000200137
visible 1

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