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1. Identity statement
Reference TypeConference Extended Abstract (Conference Proceedings)
Sitemtc-m16d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP7W/38TTPFB
Repositorysid.inpe.br/mtc-m19/2011/01.09.03.15   (restricted access)
Last Update2011:01.09.03.15.42 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m19/2011/01.09.03.15.11
Metadata Last Update2018:06.05.04.35.10 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeyGuareschiSchPetChaTam:2010:AnFiPr
TitleAnalysis of field programmable gate array alternatives for use in nanosatellites
Year2010
Access Date2024, Apr. 27
Secondary TypePRE CI
Number of Files1
Size169 KiB
2. Context
Author1 Guareschi, William N.
2 Schuch, Nelson Jorge
3 Petry, Adriano
4 Charão, Andrea Schwertner
5 Tambara, Lucas Antunes
Resume Identifier1
2 8JMKD3MGP5W/3C9JHUD
Group1
2 CRS-CCR-INPE-MCT-BR
3 CRS-CCR-INPE-MCT-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Conference NameScientific Committee on Antarctic Research (Scar) Open Science Conference.
Conference LocationPraga, Portugual
Date27th September - 1st October
Book TitleExtended Abstracts
History (UTC)2011-01-09 03:19:22 :: seeger05 -> administrator :: 2010
2018-06-05 04:35:10 :: administrator -> seeger05 :: 2010
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
AbstractMiniaturized satellites require specific design since they present serious constraints, like mass, power supply and volume. Even though simpler than bigger satellites, the electronic parts must be rigorously designed once these devices will be under severe radiation throughout their lifetime, after deployment in the Low Earth Orbit by the launcher vehicle. Nanosatellites space technology implies on development of low costs devices, and the off the shelf products would be a good alternative. Field Programmable Gate Arrays (FPGAs) have become faster, more versatile and cheaper, but still susceptible to Single Event Upset (SEU) over the space environment. The analysis of different devices is needed in order to use FPGAs in Nanosatellites. This work analyzes various FPGAs, considering available tools and documentation, power consumption, quantity of system gates, radiation tolerance and operating temperature which will be applied on the Brazilian CubeSat Project the NANOSATC-BR. These features are matched with Nanosatellites project restrictions. Preliminary results indicate that few FPGAs can be successful used on Nanosatellites projects.
AreaCEA
Arrangementurlib.net > CRCRS > Analysis of field...
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source Directory Contentthere are no files
agreement Directory Content
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4. Conditions of access and use
Languageen
Target FileIAC-10.B4.6B.12 4 Analysis of field programmable gate .... Adriano Petry.pdf
User Groupadministrator
seeger05
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
Host Collectionsid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notes
Empty Fieldsarchivingpolicy archivist 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 secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume
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