Green Propellants: Oxidizers

Detalhes bibliográficos
Autor(a) principal: Silva,Gilson da
Data de Publicação: 2013
Outros Autores: Rufino,Simone Carvalho, Iha,Koshun
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=S2175-91462013000200139
Resumo: ABSTRACT: The research for low toxicity and no damage to the environment has stimulated the development of specific investigation lines in many areas. Inevitably, the criteria for safe handling, sensitivity and, above all, specific impulse (efficiencies) of propellant compositions are still superior in relation to ecological appeals. Nowadays, however, the solid or liquid propulsion, as aerospace as military, has already compounds to efficiency and eco-friendly characteristics. This study aimed at describing “green” alternatives to propulsive systems.
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spelling Green Propellants: OxidizersPropellantAmmonium perchlorateAmmonium dinitramideHydrazinium nitroformateHydroxyl-terminated polybutadieneGlycidyl azide polymerABSTRACT: The research for low toxicity and no damage to the environment has stimulated the development of specific investigation lines in many areas. Inevitably, the criteria for safe handling, sensitivity and, above all, specific impulse (efficiencies) of propellant compositions are still superior in relation to ecological appeals. Nowadays, however, the solid or liquid propulsion, as aerospace as military, has already compounds to efficiency and eco-friendly characteristics. This study aimed at describing “green” alternatives to propulsive systems.Departamento de Ciência e Tecnologia Aeroespacial2013-06-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462013000200139Journal of Aerospace Technology and Management v.5 n.2 2013reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v5i2.229info:eu-repo/semantics/openAccessSilva,Gilson daRufino,Simone CarvalhoIha,Koshuneng2017-05-25T00:00:00Zoai:scielo:S2175-91462013000200139Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-25T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Green Propellants: Oxidizers
title Green Propellants: Oxidizers
spellingShingle Green Propellants: Oxidizers
Silva,Gilson da
Propellant
Ammonium perchlorate
Ammonium dinitramide
Hydrazinium nitroformate
Hydroxyl-terminated polybutadiene
Glycidyl azide polymer
title_short Green Propellants: Oxidizers
title_full Green Propellants: Oxidizers
title_fullStr Green Propellants: Oxidizers
title_full_unstemmed Green Propellants: Oxidizers
title_sort Green Propellants: Oxidizers
author Silva,Gilson da
author_facet Silva,Gilson da
Rufino,Simone Carvalho
Iha,Koshun
author_role author
author2 Rufino,Simone Carvalho
Iha,Koshun
author2_role author
author
dc.contributor.author.fl_str_mv Silva,Gilson da
Rufino,Simone Carvalho
Iha,Koshun
dc.subject.por.fl_str_mv Propellant
Ammonium perchlorate
Ammonium dinitramide
Hydrazinium nitroformate
Hydroxyl-terminated polybutadiene
Glycidyl azide polymer
topic Propellant
Ammonium perchlorate
Ammonium dinitramide
Hydrazinium nitroformate
Hydroxyl-terminated polybutadiene
Glycidyl azide polymer
description ABSTRACT: The research for low toxicity and no damage to the environment has stimulated the development of specific investigation lines in many areas. Inevitably, the criteria for safe handling, sensitivity and, above all, specific impulse (efficiencies) of propellant compositions are still superior in relation to ecological appeals. Nowadays, however, the solid or liquid propulsion, as aerospace as military, has already compounds to efficiency and eco-friendly characteristics. This study aimed at describing “green” alternatives to propulsive systems.
publishDate 2013
dc.date.none.fl_str_mv 2013-06-01
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=S2175-91462013000200139
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462013000200139
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v5i2.229
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.5 n.2 2013
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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