Design and Analysis of a Novel Spacecraft for Mitigating Global Warming

Detalhes bibliográficos
Autor(a) principal: He,Jie
Data de Publicação: 2018
Outros Autores: Zheng,Fei
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=S2175-91462018000100307
Resumo: ABSTRACT: A device called Huge Space Shield (HSS) has been put forward for mitigating global warming. This is a space tethers system, which use cables to connect a shielding surface and a mechanism control. In this study, orbital analysis was carried out to choose the best orbit for getting the best effect. Simulation studies were employed to understand the HSS at the beginning of entering the orbit, which were based on completely and semi-simplified model. Therefore, the force analysis gives rise to the system would not fail in the period of running on the orbit. All the results show that the HSS is stable at launch and operation, which can help ease global warming.
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spelling Design and Analysis of a Novel Spacecraft for Mitigating Global WarmingGlobal warmingOrbit selectionDeploying ability analysisForce analysisABSTRACT: A device called Huge Space Shield (HSS) has been put forward for mitigating global warming. This is a space tethers system, which use cables to connect a shielding surface and a mechanism control. In this study, orbital analysis was carried out to choose the best orbit for getting the best effect. Simulation studies were employed to understand the HSS at the beginning of entering the orbit, which were based on completely and semi-simplified model. Therefore, the force analysis gives rise to the system would not fail in the period of running on the orbit. All the results show that the HSS is stable at launch and operation, which can help ease global warming.Departamento de Ciência e Tecnologia Aeroespacial2018-01-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462018000100307Journal of Aerospace Technology and Management v.10 2018reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v10.903info:eu-repo/semantics/openAccessHe,JieZheng,Feieng2018-02-23T00:00:00Zoai:scielo:S2175-91462018000100307Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2018-02-23T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Design and Analysis of a Novel Spacecraft for Mitigating Global Warming
title Design and Analysis of a Novel Spacecraft for Mitigating Global Warming
spellingShingle Design and Analysis of a Novel Spacecraft for Mitigating Global Warming
He,Jie
Global warming
Orbit selection
Deploying ability analysis
Force analysis
title_short Design and Analysis of a Novel Spacecraft for Mitigating Global Warming
title_full Design and Analysis of a Novel Spacecraft for Mitigating Global Warming
title_fullStr Design and Analysis of a Novel Spacecraft for Mitigating Global Warming
title_full_unstemmed Design and Analysis of a Novel Spacecraft for Mitigating Global Warming
title_sort Design and Analysis of a Novel Spacecraft for Mitigating Global Warming
author He,Jie
author_facet He,Jie
Zheng,Fei
author_role author
author2 Zheng,Fei
author2_role author
dc.contributor.author.fl_str_mv He,Jie
Zheng,Fei
dc.subject.por.fl_str_mv Global warming
Orbit selection
Deploying ability analysis
Force analysis
topic Global warming
Orbit selection
Deploying ability analysis
Force analysis
description ABSTRACT: A device called Huge Space Shield (HSS) has been put forward for mitigating global warming. This is a space tethers system, which use cables to connect a shielding surface and a mechanism control. In this study, orbital analysis was carried out to choose the best orbit for getting the best effect. Simulation studies were employed to understand the HSS at the beginning of entering the orbit, which were based on completely and semi-simplified model. Therefore, the force analysis gives rise to the system would not fail in the period of running on the orbit. All the results show that the HSS is stable at launch and operation, which can help ease global warming.
publishDate 2018
dc.date.none.fl_str_mv 2018-01-01
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=S2175-91462018000100307
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462018000100307
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v10.903
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.10 2018
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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