| 1. Identificação | ||||
| Tipo de Referência | Artigo em Revista Científica (Journal Article) | |||
| Site | mtc-m21c.sid.inpe.br | |||
| Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S | |||
| Identificador | 8JMKD3MGP3W34R/442LNQ2 | |||
| Repositório | sid.inpe.br/mtc-m21c/2021/01.20.11.51 (acesso restrito) | |||
| Última Atualização | 2021:01.20.11.51.49 (UTC) simone | |||
| Repositório de Metadados | sid.inpe.br/mtc-m21c/2021/01.20.11.51.49 | |||
| Última Atualização dos Metadados | 2022:04.03.19.24.24 (UTC) administrator | |||
| DOI | 10.1016/j.asr.2020.10.024 | |||
| ISSN | 0273-1177 1879-1948 | |||
| Chave de Citação | MurciaPiñerosDosSPrad:2021:AnOrLi | |||
| Título | Analysis of the orbit lifetime of CubeSats in low Earth orbits including periodic variation in drag due to attitude motion  | |||
| Ano | 2021 | |||
| Mês | jan. | |||
| Data de Acesso | 18 maio 2024 | |||
| Tipo de Trabalho | journal article | |||
| Tipo Secundário | PRE PI | |||
| Número de Arquivos | 1 | |||
| Tamanho | 4055 KiB | |||
| 2. Contextualização | ||||
| Autor | 1 Murcia Piñeros, Jhonathan Orlando 2 Dos Santos, Walter Abrahão 3 Prado, Antonio Fernando Bertachini de Almeida | |||
| Identificador de Curriculo | 1 2 8JMKD3MGP5W/3C9JJC2 3 8JMKD3MGP5W/3C9JGJA | |||
| Grupo | 1 DIEEC-CGCE-INPE-MCTI-GOV-BR 2 DIPST-CGCE-INPE-MCTI-GOV-BR 3 DIEEC-CGCE-INPE-MCTI-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 jhonathan.pineros@inpe.br 2 walter.abrahao@inpe.br 3 antonio.prado@inpe.br | |||
| Revista | Advances in Space Research | |||
| Volume | 67 | |||
| Número | 22 | |||
| Páginas | 902-918 | |||
| Nota Secundária | B1_INTERDISCIPLINAR B1_GEOCIÊNCIAS B1_ENGENHARIAS_IV B1_ENGENHARIAS_III B1_BIODIVERSIDADE B3_CIÊNCIA_DA_COMPUTAÇÃO B4_ASTRONOMIA_/_FÍSICA C_CIÊNCIAS_BIOLÓGICAS_I | |||
| Histórico (UTC) | 2021-01-20 11:51:49 :: simone -> administrator :: 2021-01-20 11:51:55 :: administrator -> simone :: 2021 2021-01-20 11:52:32 :: simone -> administrator :: 2021 2022-04-03 19:24:24 :: administrator -> simone :: 2021 | |||
| 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 | Aerodynamic drag CubeSat Low Earth Orbits Orbit propagation Orbit decay Space debris mitigation | |||
| Resumo | It is estimated that more than 22,300 human-made objects are in orbit around the Earth, with a total mass above 8,400,000 kg. Around 89% of these objects are non-operational and without control, which makes them to be considered orbital debris. These numbers consider only objects with dimensions larger than 10 cm. Besides those numbers, there are also about 2000 operational satellites in orbit nowadays. The space debris represents a hazard to operational satellites and to the space operations. A major concern is that this number is growing, due to new launches and particles generated by collisions. Another important point is that the development of CubeSats has increased exponentially in the last years, increasing the number of objects in space, mainly in the Low Earth Orbits (LEO). Due to the short operational time, CubeSats boost the debris population. One of the requirements for space debris mitigation in LEO is the limitation of the orbital lifetime of the satellites, which needs to be lower than 25 years. However, there are space debris with longer estimated decay time. In LEO's, the influence of the atmospheric drag is the main orbital perturbation, and is used in maneuvers to increment the losses in the satellite orbital energy, to locate satellites in constellations and to accelerate the decay. The goal of the present research is to study the influence of aerodynamic rotational maneuver in the CubeSat's orbital lifetime. The rotational axis is orthogonal to the orbital plane of the CubeSat, which generates variations in the ballistic coefficient along the trajectory. The maneuver is proposed to accelerate the decay and to mitigate orbital debris generated by non-operational CubeSats. The panel method is selected to determine the drag coefficient as a function of the flow incident angle and the spinning rate. The pressure distribution is integrated from the satellite faces at hypersonic rarefied flow to calculate the drag coefficient. The mathematical model considers the gravitational potential of the Earth and the deceleration due to drag. To analyze the effects of the rotation during the decay, multiple trajectories were propagated, comparing the results obtained assuming a constant drag coefficient with trajectories where the drag coefficient changes periodically. The initial perigees selected were lower than 400 km of altitude with eccentricities ranging from 0.00 to 0.02. Six values for the angular velocity were applied in the maneuver. The technique of rotating the spacecraft is an interesting solution to increase the orbit decay of a CubeSat without implementing additional de-orbit devices. Significant changes in the decay time are presented due to the increase of the mean drag coefficient calculated by the panel method, when the maneuver is applied, reducing the orbital lifetime, however the results are independent of the angular velocity of the satellite. | |||
| Área | ETES | |||
| Arranjo | urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > Analysis of the... | |||
| 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 | ||||
| Idioma | en | |||
| Arquivo Alvo | pineros_analysis.pdf | |||
| Grupo de Usuários | simone | |||
| Grupo de Leitores | administrator simone | |||
| Visibilidade | shown | |||
| Política de Arquivamento | denypublisher denyfinaldraft24 | |||
| Permissão de Leitura | deny from all and allow from 150.163 | |||
| Permissão de Atualização | não transferida | |||
| 5. Fontes relacionadas | ||||
| Unidades Imediatamente Superiores | 8JMKD3MGPCW/46KTFK8 | |||
| Lista de Itens Citando | sid.inpe.br/mtc-m21/2012/07.13.14.40.20 2 sid.inpe.br/mtc-m21/2012/07.13.15.01.48 1 sid.inpe.br/bibdigital/2022/04.03.17.52 1 | |||
| Divulgação | WEBSCI; PORTALCAPES; COMPENDEX; SCOPUS. | |||
| Acervo Hospedeiro | urlib.net/www/2017/11.22.19.04 | |||
| 6. Notas | ||||
| Campos Vazios | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url | |||
| 7. Controle da descrição | ||||
| e-Mail (login) | simone | |||
| atualizar | ||||