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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP7W/36KUSDH
Repositorysid.inpe.br/mtc-m19@80/2009/12.24.00.43   (restricted access)
Last Update2009:12.24.00.43.46 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m19@80/2009/12.24.00.43.47
Metadata Last Update2021:02.11.18.19.19 (UTC) administrator
Citation KeyCostaSoScDuSoCoZo:2009:ThCoSu
TitleThermal control subsystem for the nanosatc-br – the first brazilian scientific cubesat
Year2009
Access Date2024, Apr. 27
Secondary TypePRE CI
Number of Files1
Size1175 KiB
2. Context
Author1 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
Resume Identifier1
2 8JMKD3MGP5W/3C9JJ48
3 8JMKD3MGP5W/3C9JHUD
4 8JMKD3MGP5W/3C9JJ2L
5 8JMKD3MGP5W/3C9JH3H
Group1 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
Affiliation1 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)
Conference NameInternational Congress of Mechanical Engineering.
Conference LocationGramado, RS
DateNovember, 15-10
Tertiary TypeFull Paper
History (UTC)2010-01-21 02:57:10 :: seeger5 -> administrator ::
2021-02-11 18:19:19 :: administrator -> seeger5 :: 2009
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
AbstractNowadays 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.
AreaCEA
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4. Conditions of access and use
Languageen
Target FileFull_Paper_Cobem_2009_LucasLCosta_Rev. Petrônio.doc
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Visibilityshown
Read Permissiondeny from all and allow from 150.163
5. Allied materials
Mirror Repositorysid.inpe.br/mtc-m19@80/2009/08.21.17.02.53
Next Higher Units8JMKD3MGPCW/3EUFCFP
8JMKD3MGPCW/444BQ9E
8JMKD3MGPCW/446AF4B
Host Collectionsid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notes
Empty Fieldsarchivingpolicy 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
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