1. Identificação | |
Tipo de Referência | Artigo em Evento (Conference Proceedings) |
Site | mtc-m21c.sid.inpe.br |
Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identificador | 8JMKD3MGP3W34R/3RTQH9H |
Repositório | sid.inpe.br/mtc-m21c/2018/10.01.16.19 |
Última Atualização | 2019:01.10.15.35.49 (UTC) administrator |
Repositório de Metadados | sid.inpe.br/mtc-m21c/2018/10.01.16.19.55 |
Última Atualização dos Metadados | 2021:02.11.18.14.24 (UTC) administrator |
Chave Secundária | INPE--PRE/ |
Chave de Citação | FerreiraMoraPradWint:2018:TeSlMa |
Título | Tethered slingshot maneuver in the three-dimensional space |
Ano | 2018 |
Data de Acesso | 05 maio 2024 |
Tipo Secundário | PRE CI |
Número de Arquivos | 1 |
Tamanho | 944 KiB |
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2. Contextualização | |
Autor | 1 Ferreira, Alessandra 2 Moraes, Rodolpho Vilhena de 3 Prado, Antonio Fernando Bertachini de Almeida 4 Winter, Othon |
Identificador de Curriculo | 1 2 3 8JMKD3MGP5W/3C9JGJA |
Grupo | 1 2 3 DIDMC-CGETE-INPE-MCTIC-GOV-BR |
Afiliação | 1 Universidade Estadual Paulista (UNESP) 2 Universidade Estadual Paulista (UNESP) 3 Instituto Nacional de Pesquisas Espaciais (INPE) 4 Universidade Estadual Paulista (UNESP) |
Endereço de e-Mail do Autor | 1 aleferrazsilva@hotmail.com 2 rodolpho.vilhena@gmail.com 3 antonio.prado@inpe.br 4 ocwinter@gmail.com |
Nome do Evento | International Astronautical Congress, 69 |
Localização do Evento | Bremen |
Data | 01-05 oct. |
Histórico (UTC) | 2018-10-01 16:19:55 :: simone -> administrator :: 2019-01-04 16:57:12 :: administrator -> simone :: 2018 2019-01-07 10:06:47 :: simone -> administrator :: 2018 2021-02-11 18:14:24 :: administrator -> simone :: 2018 |
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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 |
Resumo | The Tethered Slingshot maneuver (TSM) [1] is an alternative technique to maneuver a spacecraft in space based in the use of space tethers. A space tether used for this type of application consists in a cable where one of the ends is fixed in a celestial body (a planet, moon or asteroid) while the other end is fixed in the spacecraft that will be maneuvered. The cable is considered thin, rigid, inextensible and with negligible mass. There are several options to make this maneuver. The tether can be taken on-board the spacecraft and then fixed to the celestial body by an harpoon mechanism during the passage, or it can installed in the celestial body previously [2]. The purpose of the maneuver is the variation of energy and/or inclination in the orbit of the spacecraft around the Sun. Both aspects obtained by Tethered Slingshot Maneuver will be analyzed. The maneuver works as follows: the spacecraft approaches the body, connects to the cable that makes up the tether, rotates around the body by a given angle and, in sequence, the spacecraft is released from the cable to follow its trajectory. The rotation made in the spacecraft makes significant modifications in the trajectory of the spacecraft. The rotation from the tether and the sequential trajectory of the spacecraft is modeled in three-dimensional space, using the restricted three-body problem for improved accuracy over the usual patched-conics approach. This tethered maneuver gives flexibility to the mission, making possible for the spacecraft to reach goals that would be too expensive, in terms of fuel consumption, for a standard maneuver based only in propulsion systems. Different geometries, sizes and locations of the tether will be considered to make general maps that can guide a mission designer to get the most gains possible for the desired mission. Several examples using moons and asteroids of the Solar System will be shown. |
Área | ETES |
Arranjo | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Tethered slingshot maneuver... |
Conteúdo da Pasta doc | acessar |
Conteúdo da Pasta source | não têm arquivos |
Conteúdo da Pasta agreement | |
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4. Condições de acesso e uso | |
URL dos dados | http://urlib.net/ibi/8JMKD3MGP3W34R/3RTQH9H |
URL dos dados zipados | http://urlib.net/zip/8JMKD3MGP3W34R/3RTQH9H |
Idioma | pt |
Arquivo Alvo | IAC-ale.pdf |
Grupo de Usuários | self-uploading-INPE-MCTI-GOV-BR simone |
Visibilidade | shown |
Permissão de Atualização | não transferida |
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5. Fontes relacionadas | |
Vinculação | Trabalho não Vinculado à Tese/Dissertação |
Unidades Imediatamente Superiores | 8JMKD3MGPCW/446AF4B |
Lista de Itens Citando | sid.inpe.br/mtc-m21/2012/07.13.14.40.20 1 |
Acervo Hospedeiro | urlib.net/www/2017/11.22.19.04 |
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6. Notas | |
Campos Vazios | archivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarytype type url volume |
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7. Controle da descrição | |
e-Mail (login) | simone |
atualizar | |
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