Fechar

1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Sitemtc-m16d.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP7W/36KUSDH
Repositóriosid.inpe.br/mtc-m19@80/2009/12.24.00.43   (acesso restrito)
Última Atualização2009:12.24.00.43.46 (UTC) administrator
Repositório de Metadadossid.inpe.br/mtc-m19@80/2009/12.24.00.43.47
Última Atualização dos Metadados2021:02.11.18.19.19 (UTC) administrator
Chave de CitaçãoCostaSoScDuSoCoZo:2009:ThCoSu
TítuloThermal control subsystem for the nanosatc-br – the first brazilian scientific cubesat
Ano2009
Data de Acesso29 abr. 2024
Tipo SecundárioPRE CI
Número de Arquivos1
Tamanho1175 KiB
2. Contextualização
Autor1 Costa, Lucas Lopes
2 Souza, Petrônio Noronha de
3 Schuch, Nelson Jorge
4 Durão, Otávio Santos Cupertino
5 Sousa, Fabiano Luis de
6 Costa, Rafael Lopes
7 Zolar, Rubens Bohrer
Identificador de Curriculo1
2 8JMKD3MGP5W/3C9JJ48
3 8JMKD3MGP5W/3C9JHUD
4 8JMKD3MGP5W/3C9JJ2L
5 8JMKD3MGP5W/3C9JH3H
Grupo1 CRS-CCR-INPE-MCT-BR
2 LIT-LIT-INPE-MCT-BR
3 CRS-CCR-INPE-MCT-BR
4 DMC-ETE-INPE-MCT-BR
5 SCC-COF-INPE-MCT-BR
6 CRS-CCR-INPE-MCT-BR
7 CRS-CCR-INPE-MCT-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Instituto Nacional de Pesquisas Espaciais (INPE)
5 Instituto Nacional de Pesquisas Espaciais (INPE)
6 Instituto Nacional de Pesquisas Espaciais (INPE)
7 Instituto Nacional de Pesquisas Espaciais (INPE)
Nome do EventoInternational Congress of Mechanical Engineering.
Localização do EventoGramado, RS
DataNovember, 15-10
Tipo TerciárioFull Paper
Histórico (UTC)2010-01-21 02:57:10 :: seeger5 -> administrator ::
2021-02-11 18:19:19 :: administrator -> seeger5 :: 2009
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
ResumoNowadays satellites are essential to human society mainly on communication system and science study. The NanosatC-BR Space Weather Mission consists of an integrated program for space research and engineering development of space technologies through the integration of a CubeSat (a cubic shape satellite with 10x10x10cm and weighting no more than 1 kg of mass), the first Brazilian scientific nanosatellite. The Mission Program was conceived at the Southern Regional Space Research Center, (CRS), from the Brazilian National Institute for Space Research INPE/MCT with the involvement of undergraduate students from the Federal University of Santa Maria UFSM. The NanosatC-BR has the scientific objective to monitor in real time the Geospace, the disturbances observed at Earths magnetosphere over the Brazilian Territory, for the determination of its effects on regions such as the South Atlantic Magnetic Anomaly (SAMA) an the Ionosphere Equatorial Electrojet. The SAMA is of great significance to satellites and other spacecraft by the fact that the communication among satellites and to the Earth are affected by interference or loss of signal and all electronic satellites systems can be exposed to damage when the satellite pass through this anomaly. The mission requires the development of scientific instrumentation and, simultaneously, the design, manufacturing, qualification, integration and launch of the nanosatellite. The CubeSat has several subsystems that support and maintain the payload and all systems functioning. The requirement of the Thermal Control Subsystem is due to the aggressive environment faced in space, because abrupt changes in temperature occur frequently and sensitive electronic devices must be properly protected to maintain its operating temperature range within the required limits. In order to provide a design which meets the temperature requirements of the spacecraft, we must account for heat inputs from the Sun, the Earth, and electrical and electronic components onboard the spacecraft. The thermal design of small satellites like the NanosatC-BR is restricted due to their size and availability of energy, so it is used only passive controls without the consumption of electrical energy. The design must comply with the limits of temperature variation inside the satellite, with all possible variables. Dedicated computer programs are used, working with advanced numerical methods, which provide a real view of the interaction of space with the satellite and the internal heat exchanges.
ÁreaCEA
Arranjo 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > CRCRS > Thermal control subsystem...
Arranjo 2urlib.net > BDMCI > Fonds > Produção anterior à 2021 > COLIT > Thermal control subsystem...
Arranjo 3urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Thermal control subsystem...
Conteúdo da Pasta docacessar
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreementnão têm arquivos
4. Condições de acesso e uso
Idiomaen
Arquivo AlvoFull_Paper_Cobem_2009_LucasLCosta_Rev. Petrônio.doc
Grupo de Usuáriosadministrator
seeger5
administrator
Visibilidadeshown
Permissão de Leituradeny from all and allow from 150.163
5. Fontes relacionadas
Repositório Espelhosid.inpe.br/mtc-m19@80/2009/08.21.17.02.53
Unidades Imediatamente Superiores8JMKD3MGPCW/3EUFCFP
8JMKD3MGPCW/444BQ9E
8JMKD3MGPCW/446AF4B
Acervo Hospedeirosid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notas
Campos Vaziosarchivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination documentstage doi e-mailaddress edition editor electronicmailaddress format isbn issn keywords label lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url versiontype volume
7. Controle da descrição
e-Mail (login)seeger5
atualizar 


Fechar