1. Identificação | |
Tipo de Referência | Artigo em Revista Científica (Journal Article) |
Site | plutao.sid.inpe.br |
Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identificador | 8JMKD3MGP3W/3UGCRGD |
Repositório | sid.inpe.br/plutao/2019/12.03.13.57.11 (acesso restrito) |
Última Atualização | 2019:12.06.00.20.32 (UTC) lattes |
Repositório de Metadados | sid.inpe.br/plutao/2019/12.03.13.57.12 |
Última Atualização dos Metadados | 2021:07.28.22.22.44 (UTC) administrator |
DOI | 10.1088/1742-6596/1365/1/012011 |
ISSN | 1742-6588 |
Rótulo | lattes: 7340081273816424 3 MurciaPGuedPrad:2019:PrTrRe |
Chave de Citação | MurciaPiñerosGuedPrad:2019:PrTrRe |
Título | Propagation of the trajectories for reentry spherical debris including rotation, melting fragmentation and voxel method |
Ano | 2019 |
Data de Acesso | 28 mar. 2024 |
Tipo de Trabalho | conference paper |
Tipo Secundário | PRE PI |
Número de Arquivos | 1 |
Tamanho | 625 KiB |
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2. Contextualização | |
Autor | 1 Murcia Piñeros, Jhonathan Orlando 2 Guedes, Ulisses Thadeu Vieira 3 Prado, Antonio Fernando Bertachini de Almeida |
Identificador de Curriculo | 1 2 8JMKD3MGP5W/3C9JJAG 3 8JMKD3MGP5W/3C9JGJA |
Grupo | 1 DIDSE-CGETE-INPE-MCTIC-GOV-BR 2 DIDSE-CGETE-INPE-MCTIC-GOV-BR 3 DIDMC-CGETE-INPE-MCTIC-GOV-BR |
Afiliação | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Instituto Nacional de Pesquisas Espaciais (INPE) |
Endereço de e-Mail do Autor | 1 2 3 antonio.prado@inpe.br |
Revista | Journal of Physics: Conference Series |
Volume | 1365 |
Páginas | 012011 |
Nota Secundária | B2_INTERDISCIPLINAR B2_ENGENHARIAS_III B3_MEDICINA_II B3_GEOCIÊNCIAS B4_MATERIAIS B4_ENGENHARIAS_II B4_BIOTECNOLOGIA C_QUÍMICA C_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA C_ENGENHARIAS_IV C_ECONOMIA C_ASTRONOMIA_/_FÍSICA |
Histórico (UTC) | 2019-12-03 13:57:12 :: lattes -> administrator :: 2019-12-06 00:18:08 :: administrator -> lattes :: 2019 2019-12-06 18:20:53 :: lattes -> administrator :: 2019 2021-07-28 22:22:44 :: administrator -> simone :: 2019 |
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3. Conteúdo e estrutura | |
É a matriz ou uma cópia? | é a matriz |
Estágio do Conteúdo | concluido |
Transferível | 1 |
Tipo do Conteúdo | External Contribution |
Tipo de Versão | publisher |
Palavras-Chave | Astrodinâmica Astrodynamics Manobras Orbitais |
Resumo | It is estimated that more than 22.000 objects are in orbit around the Earth, with a total mass of 8.400.000 kg. These numbers consider only objects with dimensions above 10 cm and some non-operational, but still orbiting satellites without control (debris). The debris represent a hazard to operational satellites and aerospace operations due to the high probability of collisions. Due to the interaction of the debris with the atmosphere of the Earth and the solar activity, they began to lose energy and finally decay. During the de-orbit process, the debris fall into the Earths atmosphere at hypersonic speeds and these objects can break-up and/or be fragmented due to the aerodynamics, thermal and structural loads. It is important to obtain the trajectory and attitude of any fragment to determine the possible survival mass, impact area, hazard conditions and risks to the population, the air traffic control, and infrastructure. In this case, it is implemented a computational code to integrate the equations of motion to propagate the dynamics and kinematics of spherical debris or propellant tanks. It is also analyzed the results of trajectories with six degrees of freedom, atmospheric winds, and Magnus effect. A voxel method is implemented to analyze the tanks heat transfer, surface temperature and structures stress. To determine and observe the influence of the rotation and the Magnus force in six reentry spherical bodies, three materials are selected; aluminum alloy, due to its application in many aerospace structures; titanium and graphite epoxy I, due to their highest melting point and specific heat. Generally, these materials are used in tanks and rocket motors. More than 62 trajectories were simulated. The mathematical model and computational code were validated in three degrees of freedom. Results are compared with data from other computational tools available in the scientific literature. The results show a good approximation with reported cases of study. New results are generated in the simulations of rotational bodies, due to the influence of aerodynamic forces in the trajectory and the changes in the stagnation regions. Due to the implementation of wind and rotation of the debris, the fragments increased the survivability and the dispersion area. |
Área | ETES |
Arranjo 1 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Propagation of the... |
Arranjo 2 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDSE > Propagation of the... |
Conteúdo da Pasta doc | acessar |
Conteúdo da Pasta source | não têm arquivos |
Conteúdo da Pasta agreement | não têm arquivos |
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4. Condições de acesso e uso | |
Idioma | pt |
Arquivo Alvo | murcia_propagation.pdf |
Grupo de Usuários | lattes |
Grupo de Leitores | administrator lattes |
Visibilidade | shown |
Política de Arquivamento | denypublisher denyfinaldraft12 |
Permissão de Leitura | deny from all and allow from 150.163 |
Permissão de Atualização | não transferida |
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5. Fontes relacionadas | |
Unidades Imediatamente Superiores | 8JMKD3MGPCW/446AF4B 8JMKD3MGPCW/446AUSL |
Divulgação | WEBSCI; PORTALCAPES; COMPENDEX. |
Acervo Hospedeiro | dpi.inpe.br/plutao@80/2008/08.19.15.01 |
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6. Notas | |
Notas | XIX Brazilian Colloquium on Orbital Dynamics 2018 |
Campos Vazios | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn lineage mark mirrorrepository month nextedition number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url |
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7. Controle da descrição | |
e-Mail (login) | simone |
atualizar | |
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